Schwarzian derivative treatment of the quantum second-order supersymmetry anomaly, and coupling-constant metamorphosis

DOE Office of Scientific and Technical Information (OSTI.GOV)

Plyushchay, Mikhail S., E-mail: mikhail.plyushchay@usach.cl

A canonical quantization scheme applied to a classical supersymmetric system with quadratic in momentum supercharges gives rise to a quantum anomaly problem described by a specific term to be quadratic in Planck constant. We reveal a close relationship between the anomaly and the Schwarzian derivative, and specify a quantization prescription which generates the anomaly-free supersymmetric quantum system with second order supercharges. We also discuss the phenomenon of a coupling-constant metamorphosis that associates quantum systems with the first-order supersymmetry to the systems with the second-order supercharges.

Substrate Sorting by a Supercharged Nanoreactor

PubMed Central

2017-01-01

Compartmentalization of proteases enables spatially and temporally controlled protein degradation in cells. Here we show that an engineered lumazine synthase protein cage, which possesses a negatively supercharged lumen, can exploit electrostatic effects to sort substrates for an encapsulated protease. This proteasome-like nanoreactor preferentially cleaves positively charged polypeptides over both anionic and zwitterionic substrates, inverting the inherent substrate specificity of the guest enzyme approximately 480 fold. Our results suggest that supercharged nanochambers could provide a simple and potentially general means of conferring substrate specificity to diverse encapsulated catalysts. PMID:29278496

Calculations of the Performance of a Compression-Ignition Engine-Compressor Turbine Combination I : Performance of a Highly Supercharged Compression-Ignition Engine

NASA Technical Reports Server (NTRS)

Sanders, J. C.; Mendelson, Alexander

1945-01-01

Small high-speed single-cylinder compression-ignition engines were tested to determine their performance characteristics under high supercharging. Calculations were made on the energy available in the exhaust gas of the compression-ignition engines. The maximum power at any given maximum cylinder pressure was obtained when the compression pressure was equal to the maximum cylinder pressure. Constant-pressure combustion was found possible at an engine speed of 2200 rpm. Exhaust pressures and temperatures were determined from an analysis of indicator cards. The analysis showed that, at rich mixtures with the exhaust back pressure equal to the inlet-air pressure, there is excess energy available for driving a turbine over that required for supercharging. The presence of this excess energy indicates that a highly supercharged compression-ignition engine might be desirable as a compressor and combustion chamber for a turbine.

Alternative Computational Protocols for Supercharging Protein Surfaces for Reversible Unfolding and Retention of Stability

PubMed Central

Der, Bryan S.; Kluwe, Christien; Miklos, Aleksandr E.; Jacak, Ron; Lyskov, Sergey; Gray, Jeffrey J.; Georgiou, George; Ellington, Andrew D.; Kuhlman, Brian

2013-01-01

Reengineering protein surfaces to exhibit high net charge, referred to as “supercharging”, can improve reversibility of unfolding by preventing aggregation of partially unfolded states. Incorporation of charged side chains should be optimized while considering structural and energetic consequences, as numerous mutations and accumulation of like-charges can also destabilize the native state. A previously demonstrated approach deterministically mutates flexible polar residues (amino acids DERKNQ) with the fewest average neighboring atoms per side chain atom (AvNAPSA). Our approach uses Rosetta-based energy calculations to choose the surface mutations. Both protocols are available for use through the ROSIE web server. The automated Rosetta and AvNAPSA approaches for supercharging choose dissimilar mutations, raising an interesting division in surface charging strategy. Rosetta-supercharged variants of GFP (RscG) ranging from −11 to −61 and +7 to +58 were experimentally tested, and for comparison, we re-tested the previously developed AvNAPSA-supercharged variants of GFP (AscG) with +36 and −30 net charge. Mid-charge variants demonstrated ∼3-fold improvement in refolding with retention of stability. However, as we pushed to higher net charges, expression and soluble yield decreased, indicating that net charge or mutational load may be limiting factors. Interestingly, the two different approaches resulted in GFP variants with similar refolding properties. Our results show that there are multiple sets of residues that can be mutated to successfully supercharge a protein, and combining alternative supercharge protocols with experimental testing can be an effective approach for charge-based improvement to refolding. PMID:23741319

An investigation of the use of discharge valves and an intake control for improving the performance of N.A.C.A. Roots type supercharger

NASA Technical Reports Server (NTRS)

Schey, Oscar W; Wilson, Ernest E

1929-01-01

This report presents the results of an analytical investigation on the practicability of using mechanically operated discharge valves in conjunction with a manually operated intake control for improving the performance of N. A. C. A. Roots type superchargers. These valves, which may be either of the oscillating or rotating type, are placed in the discharge opening of the supercharger and are so shaped and synchronized with the supercharger impellers that they do not open until the air has been compressed to the delivery pressure. The intake control limits the quantity of air compressed to engine requirements by permitting the excess air to escape from the compression chamber before compression begins. The percentage power saving and the actual horsepower saved were computed for altitudes from 0 to 20,000 feet. These computations are based on the pressure-volume cards for the conventional and the modified roots type superchargers and on the results of laboratory tests of the conventional type. The use of discharge valves shows a power saving of approximately 26 per cent at a critical altitude of 20,000 feet. In addition, these valves reduce the amplitude of the discharge pulsations and increase the volumetric efficiency. With slow-speed roots blowers operating at high-pressure differences even better results would be expected. For aircraft engine superchargers operating at high speeds these discharge valves increase the performance as above, but have the disadvantages of increasing the weight and of adding a high-speed mechanism to a simple machine. (author)

A comparison of low-pressure and supercharged operation of polymer electrolyte membrane fuel cell systems for aircraft applications

NASA Astrophysics Data System (ADS)

Werner, C.; Preiß, G.; Gores, F.; Griebenow, M.; Heitmann, S.

2016-08-01

Multifunctional fuel cell systems are competitive solutions aboard future generations of civil aircraft concerning energy consumption, environmental issues, and safety reasons. The present study compares low-pressure and supercharged operation of polymer electrolyte membrane fuel cells with respect to performance and efficiency criteria. This is motivated by the challenge of pressure-dependent fuel cell operation aboard aircraft with cabin pressure varying with operating altitude. Experimental investigations of low-pressure fuel cell operation use model-based design of experiments and are complemented by numerical investigations concerning supercharged fuel cell operation. It is demonstrated that a low-pressure operation is feasible with the fuel cell device under test, but that its range of stable operation changes between both operating modes. Including an external compressor, it can be shown that the power demand for supercharging the fuel cell is about the same as the loss in power output of the fuel cell due to low-pressure operation. Furthermore, the supercharged fuel cell operation appears to be more sensitive with respect to variations in the considered independent operating parameters load requirement, cathode stoichiometric ratio, and cooling temperature. The results indicate that a pressure-dependent self-humidification control might be able to exploit the potential of low-pressure fuel cell operation for aircraft applications to the best advantage.

Reconstruction of large unilateral hemi-facial scar contractures with supercharged expanded forehead flaps based on the anterofrontal superficial temporal vessels.

PubMed

Gan, Cheng; Fan, Jincai; Liu, Liqiang; Tian, Jia; Jiao, Hu; Chen, Wenlin; Fu, Siqi; Feng, Suyun

2013-11-01

The expanded forehead flap, using temporal pedicles, has been employed extensively in facial reconstruction. To overcome the disadvantages of the traditional dual temporal pedicles, such as the limited transfer range and the short length of the flap, the distal supercharging technique can be applied to lengthen the flap and extend the transfer range, especially in the cases with a past temporal burn injury. This article aims to present an application of the distal supercharged expanded forehead flap procedure for hemi-facial reconstruction and discuss the haemodynamics of the expanded forehead flap. The tissue expander implantation and the following forehead tissue expansion were performed regularly. When the forehead skin expansion was completed, an expanded forehead flap was created and transferred to the damaged facial area with one distal temporal vessel pedicle that was anastomosed with facial vessels in a supercharged way. All patients were analysed retrospectively. From September 2009 to September 2011, eight male patients and one female patient were treated using this method. Their flaps size ranged from 20 cm × 8 cm to 30 cm × 11 cm and no flap loss occurred. Patients came in for follow-ups 9-16 months after the procedures. All the patients were satisfied with the results. The supercharging expanded forehead flap procedure can provide reliable flap vascularity due to its elastic transferring abilities. By using a distal supercharging technique, we can lengthen and widen the flap to tailor it to the defect, while also minimising the donor defect in the patients with a past temporal injury. Copyright © 2013 British Association of Plastic, Reconstructive and Aesthetic Surgeons. Published by Elsevier Ltd. All rights reserved.

The Design of Airplane-engine Superchargers

NASA Technical Reports Server (NTRS)

Von Der Null, Werner

1937-01-01

With the forms of superchargers and underlying principles of computation, delivery heads per stage of 7,000 to 8,500 meters (air column) at an effective efficiency, based on the adiabatic process, of 0.7 may be attained, the space and weight requirements being kept within reasonable limits.

14 CFR 25.1127 - Exhaust driven turbo-superchargers.

Code of Federal Regulations, 2012 CFR

2012-01-01

... flexibility between exhaust conduits and the turbine. (b) There must be provisions for lubricating the turbine and for cooling turbine parts where temperatures are critical. (c) If the normal turbo-supercharger control system malfunctions, the turbine speed may not exceed its maximum allowable value. Except for the...

14 CFR 25.1127 - Exhaust driven turbo-superchargers.

Code of Federal Regulations, 2014 CFR

2014-01-01

... flexibility between exhaust conduits and the turbine. (b) There must be provisions for lubricating the turbine and for cooling turbine parts where temperatures are critical. (c) If the normal turbo-supercharger control system malfunctions, the turbine speed may not exceed its maximum allowable value. Except for the...

14 CFR 25.1127 - Exhaust driven turbo-superchargers.

Code of Federal Regulations, 2013 CFR

2013-01-01

... flexibility between exhaust conduits and the turbine. (b) There must be provisions for lubricating the turbine and for cooling turbine parts where temperatures are critical. (c) If the normal turbo-supercharger control system malfunctions, the turbine speed may not exceed its maximum allowable value. Except for the...

75 FR 57191 - Compliance With Interstate Motor Carrier Noise Emission Standards: Exhaust Systems

Federal Register 2010, 2011, 2012, 2013, 2014

2010-09-20

... turbocharger (supercharger driven by exhaust gases) * * *.'' The language adopted by FHWA is essentially identical to that established by EPA, except that Sec. 325.91(b) specifically treats a turbocharger as a..., `` such as a turbocharger (supercharger driven by exhaust gases)'' be removed from 49 CFR 325.91(b). In...

Limits of Single-stage Compression in Centrifugal Superchargers for Aircraft

NASA Technical Reports Server (NTRS)

Kollmann, K

1940-01-01

The limits of the single-stage compression in superchargers at the present state of development are determined by five factors. 1) by the rotor material; 2) by the formation of the flow; 3) by the manufacture of double shrouded rotors; 4) by the bearing problem; 5) by the drive method.

14 CFR 23.1143 - Engine controls.

Code of Federal Regulations, 2010 CFR

2010-01-01

... 14 Aeronautics and Space 1 2010-01-01 2010-01-01 false Engine controls. 23.1143 Section 23.1143... Accessories § 23.1143 Engine controls. (a) There must be a separate power or thrust control for each engine... supercharger controls must be arranged to allow— (1) Separate control of each engine and each supercharger; and...

The Effect of Valve Timing Upon the Performance of a Supercharged Engine at Altitude and an Unsupercharged Engine at Sea Level

NASA Technical Reports Server (NTRS)

Schey, Oscar W; Biermann, Arnold E

1932-01-01

This investigation was conducted to determine the comparative effects of valve timing on the performance of an unsupercharged engine at sea level and a supercharged engine at altitude. The tests were conducted on the NACA universal test engine. The timing of the four valve events was varied over a wide range; the engine speeds were varied between 1,050 and 1,500 r.p.m.; the compression ratios were varied between 4.35:1 and 7.35:1. The conditions of exhaust pressure and carburetor pressure of a supercharged engine were simulated for altitudes between 0 and 18,000 feet. The results show that optimum valve timing for a supercharged engine at an altitude of 18,000 feet differs slightly from that for an unsupercharged engine at sea level. A small increase in power is obtained by using the optimum timing for 18,000 feet for altitudes above 5,000 feet. The timing of the intake opening and exhaust closing becomes more critical as the compression ratio is increased.

Supercharging the transverse rectus abdominis musculocutaneous flap: breast reconstruction for the overweight and obese population.

PubMed

Wu, Liza C; Iteld, Lawrence; Song, David H

2008-06-01

Autologous breast reconstruction with the transverse rectus abdominis musculocutaneous (TRAM) flap is traditionally based on either the superior epigastric vessels (pedicled) or the deep inferior system (free). In the overweight and obese population, both techniques have been shown to have increased complications of the reconstructed breast. Another alternative is supercharging the flap by anastamosing the deep inferior epigastric vessels to either the internal mammary or thoracodorsal systems. We present a single surgeon's experience with unilateral TRAM reconstructions supercharged to either the thoracodorsal vessels, the internal mammary system, or in one case, perforator vessels in overweight and obese patients. Nineteen consecutive overweight or obese patients underwent delayed or immediate, unilateral autologous breast reconstruction with supercharged TRAM flaps between November 2000 and November 2004. The patients ranged in age from 28 to 66 years (average 49) and had an average body mass index (BMI) of 29.5 (24.9-38.3). Twelve patients had a BMI between 25 and 29.9 kg/m2; 7 patients had BMI > or =30 kg/m2. Left-sided reconstructions were 13; right-sided reconstructions were 6. Supercharging was performed by anastamosing the deep inferior epigastric artery and vein to the thoracodorsal vessels, internal mammary vessels, or perforator vessels. Follow-up ranged from 6 to 54 months. There was a qualitative increase in blood flow measured by audible Doppler signals in all patients after the arterial and venous anastamoses. There were no cases of partial or complete flap loss. One patient had a hematoma and subsequently developed minor fat necrosis. One patient had an infection of the reconstructed breast. There were no donor site complications. Supercharging the TRAM flap by means of microvascular augmentation of the deep inferior epigastric vessels provides a safe and effective breast reconstruction in the overweight and obese population with no additional morbidity.

Features of the gas dynamics and local heat transfer in intake system of piston engine with supercharging

NASA Astrophysics Data System (ADS)

Plotnikov, L. V.

2017-09-01

Comparison of experimental research results of gas dynamics and instantaneous local heat transfer in the intake pipes for piston internal combustion engines (ICE) without and with supercharging are presented in the article. Studies were conducted on full-scale experimental setups in terms of gas dynamic nonstationarity, which is characteristic of piston engines. It has been established that the turbocharger installation in a gas-air system of piston internal combustion engine leads to significant differences in the patterns of change in gas-dynamic and heat transfer characteristics of flows. These data can be used in a modernization of piston engines due to installation of a turbocharger or in a development of gas-air systems for piston ICE with supercharging.

Supercharging Protein Complexes from Aqueous Solution Disrupts their Native Conformations

NASA Astrophysics Data System (ADS)

Sterling, Harry J.; Kintzer, Alexander F.; Feld, Geoffrey K.; Cassou, Catherine A.; Krantz, Bryan A.; Williams, Evan R.

2012-02-01

The effects of aqueous solution supercharging on the solution- and gas-phase structures of two protein complexes were investigated using traveling-wave ion mobility-mass spectrometry (TWIMS-MS). Low initial concentrations of m-nitrobenzyl alcohol ( m-NBA) in the electrospray ionization (ESI) solution can effectively increase the charge of concanavalin A dimers and tetramers, but at higher m-NBA concentrations, the increases in charge are accompanied by solution-phase dissociation of the dimers and up to a ~22% increase in the collision cross section (CCS) of the tetramers. With just 0.8% m-NBA added to the ESI solution of a ~630 kDa anthrax toxin octamer complex, the average charge is increased by only ~4% compared with the "native" complex, but it is sufficiently destabilized so that extensive gas-phase fragmentation occurs in the relatively high pressure regions of the TWIMS device. Anthrax toxin complexes exist in either a prechannel or a transmembrane channel state. With m-NBA, the prechannel state of the complex has the same CCS/charge ratio in the gas phase as the transmembrane channel state of the same complex formed without m-NBA, yet undergoes extensive dissociation, indicating that destabilization from supercharging occurs in the ESI droplet prior to ion formation and is not a result of Coulombic destabilization in the gas phase as a result of higher charging. These results demonstrate that the supercharging of large protein complexes is the result of conformational changes induced by the reagents in the ESI droplets, where enrichment of the supercharging reagent during droplet evaporation occurs.

Translations on USSR Military Affairs, Number 1386

DTIC Science & Technology

1978-10-16

defended; sometimes they are com- pletely bare. They must be used to penetrate boldly to the depth of the defense. When fighting for control of...stopping the fans and supercharger , turning off the electric drive of the turret, and switching on the absorbent filter air delivery system. After...the shock wave passes the mechanic-driver should turn on the supercharger , which provides delivery of decontaminated air at sur- plus pressure into

Staged combustion with piston engine and turbine engine supercharger

DOEpatents

Fischer, Larry E [Los Gatos, CA; Anderson, Brian L [Lodi, CA; O'Brien, Kevin C [San Ramon, CA

2006-05-09

A combustion engine method and system provides increased fuel efficiency and reduces polluting exhaust emissions by burning fuel in a two-stage combustion system. Fuel is combusted in a piston engine in a first stage producing piston engine exhaust gases. Fuel contained in the piston engine exhaust gases is combusted in a second stage turbine engine. Turbine engine exhaust gases are used to supercharge the piston engine.

Staged combustion with piston engine and turbine engine supercharger

DOEpatents

Fischer, Larry E [Los Gatos, CA; Anderson, Brian L [Lodi, CA; O'Brien, Kevin C [San Ramon, CA

2011-11-01

A combustion engine method and system provides increased fuel efficiency and reduces polluting exhaust emissions by burning fuel in a two-stage combustion system. Fuel is combusted in a piston engine in a first stage producing piston engine exhaust gases. Fuel contained in the piston engine exhaust gases is combusted in a second stage turbine engine. Turbine engine exhaust gases are used to supercharge the piston engine.

Supercharging an internal combustion engine by aid of a dual-rotor bi-flux axial compressor

NASA Astrophysics Data System (ADS)

Grǎdinariu, Andrei Cristian; Mihai, Ioan

2016-12-01

Internal combustion engines can be supercharged in order to enhance their performances [1-3]. Engine power is proportional to the quantity of fresh fluid introduced into the cylinder. At present, the general tendency is to try to obtain actual specific powers as high as possible, for as small as possible cylinder capacity, without increasing the generated pollution hazards. The present paper investigates the impact of replacing a centrifugal turbo-compressor with an axial double-rotor bi-flux one [4]. The proposed method allows that for the same number of cylinders, an increase in discharged airflow, accompanied by a decrease in fuel consumption. Using a program developed under the MathCad environment, the present work was aimed at studying the way temperature modifies at the end of isentropic compression under supercharging conditions. Taking into account a variation between extreme limits of the ambient temperature, its influence upon the evolution of thermal load coefficient was analyzed considering the air pressure at the compressor cooling system outlet. This analysis was completed by an exergetical study of the heat evacuated through cylinder walls in supercharged engine conditions. The conducted investigation allows verification of whether significant differences can be observed between an axial, dual-rotor, bi-flux compressor and centrifugal compressors.

Allison V–1710 Engine on a Dynamotor Stand in the Engine Research Building

NASA Image and Video Library

1943-03-21

The first research assignment specifically created for the National Advisory Committee for Aeronautics’ (NACA) new Aircraft Engine Research Laboratory was the integration of a supercharger into the Allison V–1710 engine. The military was relying on the liquid-cooled V–1710 to power several types of World War II fighter aircraft and wanted to improve the engine's speed and altitude performance. Superchargers forced additional airflow into the combustion chamber, which increased the engine’s performance resulting in greater altitudes and speeds. They also generated excess heat that affected the engine cylinders, oil, and fuel. In 1943 the military tasked the new Aircraft Engine Research Laboratory to integrate the supercharger, improve the cooling system, and remedy associated engine knock. Three Allison engines were provided to the laboratory’s research divisions. One group was tasked with improving the supercharger performance, another analyzed the effect of the increased heat on knock in the fuel, one was responsible for improving the cooling system, and another would install the new components on the engine with minimal drag penalties. The modified engines were installed on this 2000-horsepower dynamotor stand in a test cell within the Engine Research Building. The researchers could run the engine at different temperatures, fuel-air ratios, and speeds. When the modifications were complete, the improved V–1710 was flight tested on a P–63A Kingcobra loaned to the NACA for this project.

Reconstruction of Anterolateral Thigh Defects Using Perforator-Based Propeller Flaps.

PubMed

Iida, Takuya; Yoshimatsu, Hidehiko; Koshima, Isao

2017-10-01

Usually, anterolateral thigh (ALT) defects with width more than 8 cm cannot be closed directly. Although several methods of using local flaps exist, flap mobility of these methods is limited. We introduced a perforator-based propeller flap for such reconstruction. Their maximal mobility, which minimizes their size, is their greatest advantage. In addition, we present our technical refinements including double-axes propeller flap, the use of indocyanine green real-time angiography, and supercharged propeller flap for safer flap transfer. Seven patients underwent perforator-based propeller flap reconstruction of ALT defects. Flaps were designed cranial or caudal to the defect according to the perforator locations. To maximize mobility, flaps were designed so that the perforator was located at the periphery and closer to the defect. After rotating the flap to the defect, indocyanine green angiography was performed to determine the need for supercharge. In all cases, all flaps survived completely. Defect size ranged from 12 × 11 cm to 18 × 16 cm, and flap size ranged from 7 × 5 cm to 15 × 7 cm. The number of perforators in the flap was 1 in 3 cases and 2 in 4 cases. Supercharging was performed in 3 cases. Donor-site complications, including gait disturbance, were not observed. This method achieves ALT defect closure with minimal donor-site morbidity and can provide prompt and aesthetically acceptable results. Indocyanine green real-time angiography and supercharging technique are also useful for safer and reliable flap transfer.

The comparative performance of Roots type aircraft engine superchargers as affected by change in impeller speed and displacement

NASA Technical Reports Server (NTRS)

Ware, Marsden; Wilson, Ernest E

1929-01-01

This report presents the results of tests made on three sizes of roots type aircraft engine superchargers. The impeller contours and diameters of these machines were the same, but the length were 11, 8 1/4, and 4 inches, giving displacements of 0.509, 0.382, and 0.185 cubic foot per impeller revolution. The information obtained serves as a basis for the examination of the individual effects of impeller speed and displacement on performance and of the comparative performance when speed and displacement are altered simultaneously to meet definite service requirements. According to simple theory, when assuming no losses, the air weight handled and the power required for a given pressure difference are directly proportional to the speed and the displacement. These simple relations are altered considerably by the losses. When comparing the performance of different sizes of machines whose impeller speeds are so related that the same service requirements are met, it is found that the individual effects of speed and displacement are canceled to a large extent, and the only considerable difference is the difference in the power losses which decrease with increase in the displacement and the accompanying decrease in speed. This difference is small in relation to the net power of the engine supercharger unit, so that a supercharger with short impellers may be used in those applications where the space available is very limited with any considerable sacrifice in performance.

Supersymmetric Sachdev-Ye-Kitaev models

DOE PAGES

Fu, Wenbo; Gaiotto, Davide; Maldacena, Juan; ...

2017-01-13

We discuss a supersymmetric generalization of the Sachdev-Ye-Kitaev (SYK) model. These are quantum mechanical models involving N Majorana fermions. The supercharge is given by a polynomial expression in terms of the Majorana fermions with random coefficients. The Hamiltonian is the square of the supercharge. The N = 1 model with a single supercharge has unbroken supersymmetry at large N , but nonperturbatively spontaneously broken supersymmetry in the exact theory. We analyze the model by looking at the large N equation, and also by performing numerical computations for small values of N . We also compute the large N spectrum ofmore » “singlet” operators, where we find a structure qualitatively similar to the ordinary SYK model. We also discuss an N = 2 version. In this case, the model preserves supersymmetry in the exact theory and we can compute a suitably weighted Witten index to count the number of ground states, which agrees with the large N computation of the entropy. In both cases, we discuss the supersymmetric generalizations of the Schwarzian action which give the dominant effects at low energies.« less

EVOLUTION of the Pressure Wave Supercharger Concept

NASA Astrophysics Data System (ADS)

Costiuc, Iuliana; Chiru, Anghel

2017-10-01

Born more than a century ago, the concept of exploiting the pressure wave phenomenon has evolved with rather small steps, experiencing an accelerated progress over the past decades. This paper aims an overview on the researchers’ results over time regarding the pressure wave technology and its applications, pointing out on the internal combustion engine’s supercharging application. This review complements the past reports on the subject, presenting the evolution of the concept and technology, as well as the researcher’s efforts on solving the specific shortcomings of this pressure wave technology. Undoubtedly, the pressure wave rotors have been a research goal over the years. At first, most of the researches were experimental and the theoretical calculations required to improve the technology were too arduous. Recently, new computer software dedicated to accurate simulation of the processes governing the wave rotor operation, altogether with modern experimental measurement instruments and well-developed diagnostic techniques have opened wide possibilities to innovate the pressure wave supercharging technology. This paper also highlights the challenges that specialists still have to overcome and aspects to become future preoccupations and research directions.

Solution of second order supersymmetrical intertwining relations in Minkowski plane

DOE Office of Scientific and Technical Information (OSTI.GOV)

Ioffe, M. V., E-mail: m.ioffe@spbu.ru; Kolevatova, E. V., E-mail: e.v.kolev@yandex.ru; Nishnianidze, D. N., E-mail: cutaisi@yahoo.com

2016-08-15

Supersymmetrical (SUSY) intertwining relations are generalized to the case of quantum Hamiltonians in Minkowski space. For intertwining operators (supercharges) of second order in derivatives, the intertwined Hamiltonians correspond to completely integrable systems with the symmetry operators of fourth order in momenta. In terms of components, the intertwining relations correspond to the system of nonlinear differential equations which are solvable with the simplest—constant—ansatzes for the “metric” matrix in second order part of the supercharges. The corresponding potentials are built explicitly both for diagonalizable and nondiagonalizable form of “metric” matrices, and their properties are discussed.

Simulation research on the effect of cooled EGR, supercharging and compression ratio on downsized SI engine knock

NASA Astrophysics Data System (ADS)

Shu, Gequn; Pan, Jiaying; Wei, Haiqiao; Shi, Ning

2013-03-01

Knock in spark-ignition(SI) engines severely limits engine performance and thermal efficiency. The researches on knock of downsized SI engine have mainly focused on structural design, performance optimization and advanced combustion modes, however there is little for simulation study on the effect of cooled exhaust gas recirculation(EGR) combined with downsizing technologies on SI engine performance. On the basis of mean pressure and oscillating pressure during combustion process, the effect of different levels of cooled EGR ratio, supercharging and compression ratio on engine dynamic and knock characteristic is researched with three-dimensional KIVA-3V program coupled with pressure wave equation. The cylinder pressure, combustion temperature, ignition delay timing, combustion duration, maximum mean pressure, and maximum oscillating pressure at different initial conditions are discussed and analyzed to investigate potential approaches to inhibiting engine knock while improving power output. The calculation results of the effect of just cooled EGR on knock characteristic show that appropriate levels of cooled EGR ratio can effectively suppress cylinder high-frequency pressure oscillations without obvious decrease in mean pressure. Analysis of the synergistic effect of cooled EGR, supercharging and compression ratio on knock characteristic indicates that under the condition of high supercharging and compression ratio, several times more cooled EGR ratio than that under the original condition is necessarily utilized to suppress knock occurrence effectively. The proposed method of synergistic effect of cooled EGR and downsizing technologies on knock characteristic, analyzed from the aspects of mean pressure and oscillating pressure, is an effective way to study downsized SI engine knock and provides knock inhibition approaches in practical engineering.

Learning Physics with Digital Game Simulations in Middle School Science

NASA Astrophysics Data System (ADS)

Anderson, Janice L.; Barnett, Mike

2013-12-01

The purpose of this work is to share our findings in using video gaming technology to facilitate the understanding of basic electromagnetism with middle school students. To this end, we explored the impact of using a game called Supercharged! on middle school students' understanding of electromagnetic concepts compared to students who conducted a more traditional inquiry-oriented investigation of the same concepts. This study was a part of a larger design experiment examining the pedagogical potential of Supercharged! The control group learned through a series of guided inquiry methods while the experimental group played Supercharged! during the laboratory sections of the science course. There was significant difference, F(2,91) = 3.6, p < 0.05, η 2 = 0.77, between the control and experimental groups on the gains from pre- to post-assessment. Additionally, students in the experimental group were able to give more nuanced responses about the descriptions of electric fields and the influence of distance on the forces that charges experience due to their interactions with the Supercharged! game. Results of this study show that video games can lead to positive learning outcomes, as demonstrated by the increase in test scores from pre- to post-assessment and the student interviews. This study also suggests that a complementary approach, in which video games and hands-on activities are integrated, with each activity informing the other, could be a very powerful technique for supporting student scientific understanding. Further, our findings suggest that game designers should embed meta-cognitive activities such as reflective opportunities into educational video games in order to provide scaffolds for students and to reinforce that they are engaged in an educational learning experience.

Performance of a supercharged direct-injection stratified-charge rotary combustion engine

NASA Technical Reports Server (NTRS)

Bartrand, Timothy A.; Willis, Edward A.

1990-01-01

A zero-dimensional thermodynamic performance computer model for direct-injection stratified-charge rotary combustion engines was modified and run for a single rotor supercharged engine. Operating conditions for the computer runs were a single boost pressure and a matrix of speeds, loads and engine materials. A representative engine map is presented showing the predicted range of efficient operation. After discussion of the engine map, a number of engine features are analyzed individually. These features are: heat transfer and the influence insulating materials have on engine performance and exhaust energy; intake manifold pressure oscillations and interactions with the combustion chamber; and performance losses and seal friction. Finally, code running times and convergence data are presented.

Improved liquid chromatography-MS/MS of heparan sulfate oligosaccharides via chip-based pulsed makeup flow.

PubMed

Huang, Yu; Shi, Xiaofeng; Yu, Xiang; Leymarie, Nancy; Staples, Gregory O; Yin, Hongfeng; Killeen, Kevin; Zaia, Joseph

2011-11-01

Microfluidic chip-based hydrophilic interaction chromatography (HILIC) is a useful separation system for liquid chromatography-mass spectrometry (LC-MS) in compositional profiling of heparan sulfate (HS) oligosaccharides; however, ions observed using HILIC LC-MS are low in charge. Tandem MS of HS oligosaccharide ions with low charge results in undesirable losses of SO(3) from precursor ions during collision induced dissociation. One solution is to add metal cations to stabilize sulfate groups. Another is to add a nonvolatile, polar compound such as sulfolane, a molecule known to supercharge proteins, to produce a similar effect for oligosaccharides. We demonstrate use of a novel pulsed makeup flow (MUF) HPLC-chip. The chip enables controlled application of additives during specified chromatographic time windows and thus minimizes the extent to which nonvolatile additives build up in the ion source. The pulsed MUF system was applied to LC-MS/MS of HS oligosaccharides. Metal cations and sulfolane were tested as additives. The most promising results were obtained for sulfolane, for which supercharging of the oligosaccharide ions increased their signal strengths relative to controls. Tandem MS of these supercharged precursor ions showed decreased abundances of product ions from sulfate losses yet more abundant product ions from backbone cleavages.

Full action of two deformation operators in the D1D5 CFT

NASA Astrophysics Data System (ADS)

Carson, Zaq; Hampton, Shaun; Mathur, Samir D.

2017-11-01

We are interested in thermalization in the D1D5 CFT, since this process is expected to be dual to black hole formation. We expect that the lowest order process where thermalization occurs will be at second order in the perturbation that moves us away from the orbifold point. The operator governing the deformation off of the orbifold point consists of a twist operator combined with a supercharge operator acting on this twist. In a previous paper we computed the action of two twist operators on an arbitrary state of the CFT. In the present work we compute the action of the supercharges on these twist operators, thereby obtaining the full action of two deformation operators on an arbitrary state of the CFT. We show that the full amplitude can be related to the amplitude with just the twists through an action of the supercharge operators on the initial and final states. The essential part of this computation consists of moving the contours from the twist operators to the initial and final states; to do this one must first map the amplitude to a covering space where the twists are removed, and then map back to the original space on which the CFT is defined.

Real-time HD Exchange Kinetics of Proteins from Buffered Aqueous Solution with Electrothermal Supercharging and Top-Down Tandem Mass Spectrometry

NASA Astrophysics Data System (ADS)

Going, Catherine C.; Xia, Zijie; Williams, Evan R.

2016-06-01

Electrothermal supercharging (ETS) with electrospray ionization produces highly charged protein ions from buffered aqueous solutions in which proteins have native folded structures. ETS increases the charge of ribonuclease A by 34%, whereas only a 6% increase in charge occurs for a reduced-alkylated form of this protein, which is unfolded and its structure is ~66% random coil in this solution. These results indicate that protein denaturation that occurs in the ESI droplets is the primary mechanism for ETS. ETS does not affect the extent of solution-phase hydrogen-deuterium exchange (HDX) that occurs for four proteins that have significantly different structures in solution, consistent with a droplet lifetime that is considerably shorter than observable rates of HDX. Rate constants for HDX of ubiquitin are obtained with a spatial resolution of ~1.3 residues with ETS and electron transfer dissociation of the 10+ charge-state using a single capillary containing a few μL of protein solution in which HDX continuously occurs. HDX protection at individual residues with ETS HDX is similar to that with reagent supercharging HDX and with solution-phase NMR, indicating that the high spray potentials required to induce ETS do not lead to HD scrambling.

The Use of Chromium(III) to Supercharge Peptides by Protonation at Low Basicity Sites

NASA Astrophysics Data System (ADS)

Feng, Changgeng; Commodore, Juliette J.; Cassady, Carolyn J.

2015-02-01

The addition of chromium(III) nitrate to solutions of peptides with seven or more residues greatly increases the formation of doubly protonated peptides, [M + 2H]2+, by electrospray ionization. The test compound heptaalanine has only one highly basic site (the N-terminal amino group) and undergoes almost exclusive single protonation using standard solvents. When Cr(III) is added to the solution, abundant [M + 2H]2+ forms, which involves protonation of the peptide backbone or the C-terminus. Salts of Al(III), Mn(II), Fe(III), Fe(II), Cu(II), Zn (II), Rh(III), La(III), Ce(IV), and Eu(III) were also studied. Although several metal ions slightly enhance protonation, Cr(III) has by far the greatest ability to generate [M + 2H]2+. Cr(III) does not supercharge peptide methyl esters, which suggests that the mechanism involves interaction of Cr(III) with a carboxylic acid group. Other factors may include the high acidity of hexa-aquochromium(III) and the resistance of Cr(III) to reduction. Nitrate salts enhance protonation more than chloride salts and a molar ratio of 10:1 Cr(III):peptide produces the most intense [M + 2H]2+. Cr(III) also supercharges numerous other small peptides, including highly acidic species. For basic peptides, Cr(III) increases the charge state (2+ versus 1+) and causes the number of peptide molecules being protonated to double or triple. Chromium(III) does not supercharge the proteins cytochrome c and myoglobin. The ability of Cr(III) to enhance [M + 2H]2+ intensity may prove useful in tandem mass spectrometry because of the resulting overall increase in signal-to-noise ratio, the fact that [M + 2H]2+ generally dissociate more readily than [M + H]+, and the ability to produce [M + 2H]2+ precursors for electron-based dissociation techniques.

14 CFR 145.59 - Ratings.

Code of Federal Regulations, 2011 CFR

2011-01-01

... tubes, transistors, or similar devices, including capacitance type quantity gauges, system amplifiers... depends on the use of an electron tube transistor, or similar device, including supercharger, temperature...

14 CFR 145.59 - Ratings.

Code of Federal Regulations, 2012 CFR

2012-01-01

... tubes, transistors, or similar devices, including capacitance type quantity gauges, system amplifiers... depends on the use of an electron tube transistor, or similar device, including supercharger, temperature...

14 CFR 145.59 - Ratings.

Code of Federal Regulations, 2013 CFR

2013-01-01

... tubes, transistors, or similar devices, including capacitance type quantity gauges, system amplifiers... depends on the use of an electron tube transistor, or similar device, including supercharger, temperature...

14 CFR 145.59 - Ratings.

Code of Federal Regulations, 2014 CFR

2014-01-01

... tubes, transistors, or similar devices, including capacitance type quantity gauges, system amplifiers... depends on the use of an electron tube transistor, or similar device, including supercharger, temperature...

Rigid supersymmetric backgrounds of 3-dimensional Newton-Cartan supergravity

DOE PAGES

Knodel, Gino; Lisbao, Pedro; Liu, James T.

2016-06-06

Recently, a non-relativistic off-shell formulation of three dimensional Newton-Cartan supergravity was proposed as the c → ∞ limit of three dimensional N = 2 super-gravity [1]. Here in the present paper we study supersymmetric backgrounds within this theory. Using integrability constraints for the non-relativistic Killing spinor equations, we explicitly construct all maximally supersymmetric solutions, which admit four supercharges. In addition to these solutions, there aremore » $$\\frac{1}{2}$$ -BPS solutions with reduced supersymmetry. We give explicit examples of such backgrounds and derive necessary conditions for backgrounds preserving two supercharges. Finally, we address how supersymmetric backgrounds of N = 2 supergravity are connected to the solutions found here in the c → ∞ limit.« less

Bell P–63A King Cobra at the Aircraft Engine Research Laboratory

NASA Image and Video Library

1944-01-21

The Army Air Forces lent the National Advisory Committee for Aeronautics (NACA) Aircraft Engine Research Laboratory a Bell P–63A King Cobra in October 1943 to complement the lab's extensive efforts to improve the Allison V–1710 engine. The V–1710-powered P–63A was a single-seat fighter that could reach speeds of 410 miles per hour and an altitude of 43,000 feet. The fighter, first produced in 1942, was an improvement on Bell’s P–39, but persistent performance problems at high altitudes prevented its acceptance by the Air Corps. Instead many of the P–63s were transferred to the Soviet Union. Almost every test facility at the NACA’s engine lab was used to study the Allison V–1710 engine and its supercharger during World War II. Researchers were able to improve the efficiency, capacity and pressure ratio of the supercharger. They found that improved cooling significantly reduced engine knock in the fuel. Once the researchers were satisfied with their improvements, the new supercharger and cooling components were installed on the P–63A. The Flight Research Division first established the aircraft’s normal flight performance parameters such as speed at various altitudes, rate of climb, and peak altitude. Ensuing flights established the performance parameters of the new configuration in order to determine the improved performance. The program increased V–1710’s horsepower from 1650 to 2250.

Germany Briefing

DTIC Science & Technology

2011-07-27

Ion Battery Packs Advanced Chemistry Batteries EM Armor Power Brick 8 UNCLASSIFIED Concepts Platform Simulation Component Development Vehicle...Advanced Turbocharging, Supercharging, OPOC Efficient Powertrain Technologies Electrified Accessories Energy Harvesting SiC Electronics Lithium

Controlled Supramolecular Self-Assembly of Super-charged β-Lactoglobulin A-PEG Conjugates into Nanocapsules.

PubMed

Khan, Amit Kumar; Gudlur, Sushanth; de Hoog, Hans-Peter M; Siti, Winna; Liedberg, Bo; Nallani, Madhavan

2017-09-18

The synthesis and characterization of a new protein-polymer conjugate composed of β lactoglobulin A (βLG A) and poly(ethylene glycol) PEG is described. βLG A was selectively modified to self-assemble by super-charging via amination or succinylation followed by conjugation with PEG. An equimolar mixture of the oppositely charged protein-polymer conjugates self-assemble into spherical capsules of 80-100 nm in diameter. The self-assembly proceeds by taking simultaneous advantage of the amphiphilicity and polyelectrolyte nature of the protein-polymer conjugate. These protein-polymer capsules or proteinosomes are reminiscent of protein capsids, and are capable of encapsulating solutes in their interior. We envisage this approach to be applicable to other globular proteins. © 2017 Wiley-VCH Verlag GmbH & Co. KGaA, Weinheim.

Effect of a part-span variable inlet guide vane on the performance of a high-bypass turbofan engine

NASA Technical Reports Server (NTRS)

Bobula, G. A.; Soeder, R. H.; Burkardt, L. A.

1981-01-01

The ability of a part span variable inlet guide vane (VIGV) to modulate the thrust of a high bypass turbofan engine was evaluated at altitude/Mach number conditions of 4572 m/0.6 and 9144 m/0.93. Fan tip, gas generator and supercharger performance were also determined, both on operating lines and during fan duct throttling. The evaluation was repeated with the bypass splitter extended forward to near the fan blade trailing edge. Gross thrust attentuation of over 50 percent was achieved with 50 degree VIGV closure at 100 percent corrected fan speed. Gas generator supercharger performance fell off with VIGV closure, but this loss was reduced when a splitter extension was added. The effect of VIVG closure on gas generator performance was minimal.

Experimental Study on Relationship between NOx Emission and Fuel Consumption of a Diesel Engine

NASA Astrophysics Data System (ADS)

Ning, Ping; Liu, Chunjiang; Feng, Zhiqiang; Xia, Yijiang

2018-01-01

For YC6112 diesel engine assembled Delphl model single fuel pump electric controlled, in the premise of not changing its overall unit structure parameters of other systems, three different types of camshaft for single pumps, two kinds of fuel injectors, two types of superchargers and some phase shifting angle of different camshafts were chosen to match with the engine precisely, the experiments under thirteen kinds of working conditions for the engine with different matching were carried out, the change regulation between NOX emission and fuel consumption for the engine with different kinds of configurations was analyzed. The experiment results show the NOX emission and fuel consumption can be reduced greatly by configuring proper camshaft, fuel injectors and superchargers with YC6112 diesel engine.

Superconformal Baryon-Meson Symmetry and Light-Front Holographic QCD

DOE PAGES

Dosch, Hans Guenter; de Teramond, Guy F.; Brodsky, Stanley J.

2015-04-10

We construct an effective QCD light-front Hamiltonian for both mesons and baryons in the chiral limit based on the generalized supercharges of a superconformal graded algebra. The superconformal construction is shown to be equivalent to a semi-classical approximation to light-front QCD and its embedding in AdS space. The specific breaking of conformal invariance inside the graded algebra uniquely determines the effective confinement potential. The generalized supercharges connect the baryon and meson spectra to each other in a remarkable manner. In particular, the π/b 1 Regge trajectory is identified as the superpartner of the nucleon trajectory. However, the lowest-lying state onmore » this trajectory, the π-meson is massless in the chiral limit and has no supersymmetric partner.« less

Influence of Sulfolane on ESI-MS Measurements of Protein-Ligand Affinities

NASA Astrophysics Data System (ADS)

Yao, Yuyu; Richards, Michele R.; Kitova, Elena N.; Klassen, John S.

2016-03-01

The results of an investigation into the influence of sulfolane, a commonly used supercharging agent, on electrospray ionization mass spectrometry (ESI-MS) measurements of protein-ligand affinities are described. Binding measurements carried out on four protein-carbohydrate complexes, lysozyme with β- d-GlcNAc-(1→4)-β- d-GlcNAc-(1→4)-β- d-GlcNAc-(1→4)- d-GlcNAc, a single chain variable fragment and α- d-Gal-(1→2)-[α- d-Abe-(1→3)]-α- d-Man-OCH3, cholera toxin B subunit homopentamer with β- d-Gal-(1→3)-β- d-GalNAc-(1→4)[α- d-Neu5Ac-(2→3)]-β- d-Gal-(1→4)-β- d-Glc, and a fragment of galectin 3 and α- l-Fuc-(1→2)-β- d-Gal-(1→3)-β- d-GlcNAc-(1→3)-β- d-Gal-(1→4)-β- d-Glc, revealed that sulfolane generally reduces the apparent (as measured by ESI-MS) protein-ligand affinities. To establish the origin of this effect, a detailed study was undertaken using the lysozyme-tetrasaccharide interaction as a model system. Measurements carried out using isothermal titration calorimetry (ITC), circular dichroism, and nuclear magnetic resonance spectroscopies reveal that sulfolane reduces the binding affinity in solution but does not cause any significant change in the higher order structure of lysozyme or to the intermolecular interactions. These observations confirm that changes to the structure of lysozyme in bulk solution are not responsible for the supercharging effect induced by sulfolane. Moreover, the agreement between the ESI-MS and ITC-derived affinities indicates that there is no dissociation of the complex during ESI or in the gas phase (i.e., in-source dissociation). This finding suggests that supercharging of lysozyme by sulfolane is not related to protein unfolding during the ESI process. Binding measurements performed using liquid sample desorption ESI-MS revealed that protein supercharging with sulfolane can be achieved without a reduction in affinity.

Influence of Sulfolane on ESI-MS Measurements of Protein-Ligand Affinities.

PubMed

Yao, Yuyu; Richards, Michele R; Kitova, Elena N; Klassen, John S

2016-03-01

The results of an investigation into the influence of sulfolane, a commonly used supercharging agent, on electrospray ionization mass spectrometry (ESI-MS) measurements of protein-ligand affinities are described. Binding measurements carried out on four protein-carbohydrate complexes, lysozyme with β-D-GlcNAc-(1→4)-β-D-GlcNAc-(1→4)-β-D-GlcNAc-(1→4)-D-GlcNAc, a single chain variable fragment and α-D-Gal-(1→2)-[α-D-Abe-(1→3)]-α-D-Man-OCH3, cholera toxin B subunit homopentamer with β-D-Gal-(1→3)-β-D-GalNAc-(1→4)[α-D-Neu5Ac-(2→3)]-β-D-Gal-(1→4)-β-D-Glc, and a fragment of galectin 3 and α-L-Fuc-(1→2)-β-D-Gal-(1→3)-β-D-GlcNAc-(1→3)-β-D-Gal-(1→4)-β-D-Glc, revealed that sulfolane generally reduces the apparent (as measured by ESI-MS) protein-ligand affinities. To establish the origin of this effect, a detailed study was undertaken using the lysozyme-tetrasaccharide interaction as a model system. Measurements carried out using isothermal titration calorimetry (ITC), circular dichroism, and nuclear magnetic resonance spectroscopies reveal that sulfolane reduces the binding affinity in solution but does not cause any significant change in the higher order structure of lysozyme or to the intermolecular interactions. These observations confirm that changes to the structure of lysozyme in bulk solution are not responsible for the supercharging effect induced by sulfolane. Moreover, the agreement between the ESI-MS and ITC-derived affinities indicates that there is no dissociation of the complex during ESI or in the gas phase (i.e., in-source dissociation). This finding suggests that supercharging of lysozyme by sulfolane is not related to protein unfolding during the ESI process. Binding measurements performed using liquid sample desorption ESI-MS revealed that protein supercharging with sulfolane can be achieved without a reduction in affinity.

Some Notes on Gasoline-Engine Development

NASA Technical Reports Server (NTRS)

Ricardo, H R

1927-01-01

Experiments were carried out using a special engine with small glass windows and a stroboscope to record various aspects of engine performance. Valve position, supercharging, and torque recoil were all investigated with this experimental apparatus.

Complex coacervation of supercharged proteins with polyelectrolytes.

PubMed

Obermeyer, Allie C; Mills, Carolyn E; Dong, Xue-Hui; Flores, Romeo J; Olsen, Bradley D

2016-04-21

Complexation of proteins with polyelectrolytes or block copolymers can lead to phase separation to generate a coacervate phase or self-assembly of coacervate core micelles. However, many proteins do not coacervate at conditions near neutral pH and physiological ionic strength. Here, protein supercharging is used to systematically explore the effect of protein charge on the complex coacervation with polycations. Four model proteins were anionically supercharged to varying degrees as quantified by mass spectrometry. Proteins phase separated with strong polycations when the ratio of negatively charged residues to positively charged residues on the protein (α) was greater than 1.1-1.2. Efficient partitioning of the protein into the coacervate phase required larger α (1.5-2.0). The preferred charge ratio for coacervation was shifted away from charge symmetry for three of the four model proteins and indicated an excess of positive charge in the coacervate phase. The composition of protein and polymer in the coacervate phase was determined using fluorescently labeled components, revealing that several of the coacervates likely have both induced charging and a macromolecular charge imbalance. The model proteins were also encapsulated in complex coacervate core micelles and micelles formed when the protein charge ratio α was greater than 1.3-1.4. Small angle neutron scattering and transmission electron microscopy showed that the micelles were spherical. The stability of the coacervate phase in both the bulk and micelles improved to increased ionic strength as the net charge on the protein increased. The micelles were also stable to dehydration and elevated temperatures.

14 CFR 23.1193 - Cowling and nacelle.

Code of Federal Regulations, 2013 CFR

2013-01-01

... resist any vibration, inertia, and air loads to which it may be subjected in operation. (b) There must be... multiengine airplane with supercharged engines must be designed and constructed so that with the landing gear...

14 CFR 23.1193 - Cowling and nacelle.

Code of Federal Regulations, 2010 CFR

2010-01-01

... resist any vibration, inertia, and air loads to which it may be subjected in operation. (b) There must be... multiengine airplane with supercharged engines must be designed and constructed so that with the landing gear...

14 CFR 23.1193 - Cowling and nacelle.

Code of Federal Regulations, 2011 CFR

2011-01-01

... resist any vibration, inertia, and air loads to which it may be subjected in operation. (b) There must be... multiengine airplane with supercharged engines must be designed and constructed so that with the landing gear...

14 CFR 23.1193 - Cowling and nacelle.

Code of Federal Regulations, 2014 CFR

2014-01-01

... resist any vibration, inertia, and air loads to which it may be subjected in operation. (b) There must be... multiengine airplane with supercharged engines must be designed and constructed so that with the landing gear...

Controlled Fission: Teaching Supercharged Subjects.

ERIC Educational Resources Information Center

Pace, David

2003-01-01

Shaping classroom experiences before controversial material is encountered in a class increases the likelihood that students will maintain higher mental function while examining that material. Presents 10 strategies for planning a course that facilitates quality discussion and thoughtful debate. (SLD)

Engine Would Recover Exhaust Energy More Efficiently

NASA Technical Reports Server (NTRS)

Dimpelfeld, Philip M.

1993-01-01

Exhaust energy used for supercharging and extra shaft power. Flow of exhaust apportioned by waste gate to meet demand of turbocharger, and portion not fed to turbocharger sent to power-recovery turbine. Expected to increase fuel efficiency.

14 CFR 33.51 - Operation test.

Code of Federal Regulations, 2012 CFR

2012-01-01

... STANDARDS: AIRCRAFT ENGINES Block Tests; Reciprocating Aircraft Engines § 33.51 Operation test. The... characteristics, starting, idling, acceleration, overspeeding, functioning of propeller and ignition, and any other operational characteristic of the engine. If the engine incorporates a multispeed supercharger...

14 CFR 33.51 - Operation test.

Code of Federal Regulations, 2011 CFR

2011-01-01

... STANDARDS: AIRCRAFT ENGINES Block Tests; Reciprocating Aircraft Engines § 33.51 Operation test. The... characteristics, starting, idling, acceleration, overspeeding, functioning of propeller and ignition, and any other operational characteristic of the engine. If the engine incorporates a multispeed supercharger...

Marquardt's Mach 4.5 Supercharged Ejector Ramjet (SERJ) High-Performance Aircraft Engine Project: Unfulfilled Aspirations Ca.1970

NASA Technical Reports Server (NTRS)

Escher, William J. D.; Roddy, Jordan E.; Hyde, Eric H.

2000-01-01

The Supercharged Ejector Ramjet (SERJ) engine developments of the 1960s, as pursued by The Marquardt Corporation and its associated industry team members, are described. In just three years, engineering work on this combined-cycle powerplant type evolved, from its initial NASA-sponsored reusable space transportation system study status, into a U.S. Air Force/Navy-supported exploratory development program as a candidate 4.5 high-performance military aircraft engine. Bridging a productive transition from the spaceflight to the aviation arena, this case history supports the expectation that fully-integrated airbreathing/rocket propulsion systems hold high promise toward meeting the demanding propulsion requirements of tomorrow's aircraft-like Spaceliner class transportation systems. Lessons to be learned from this "SERJ Story" are offered for consideration by today's advanced space transportation and combined-cycle propulsion researchers and forward-planning communities.

Grain-scale supercharging and breakdown on airless regoliths

NASA Astrophysics Data System (ADS)

Zimmerman, M. I.; Farrell, W. M.; Hartzell, C. M.; Wang, X.; Horanyi, M.; Hurley, D. M.; Hibbitts, K.

2016-10-01

Interactions of the solar wind and emitted photoelectrons with airless bodies have been studied extensively. However, the details of how charged particles interact with the regolith at the scale of a single grain have remained largely uncharacterized. Recent efforts have focused upon determining total surface charge under photoemission and solar wind bombardment and the associated electric field and potential. In this work, theory and simulations are used to show that grain-grain charge differences can exceed classical sheath predictions by several orders of magnitude, sometimes reaching dielectric breakdown levels. Temperature-dependent electrical conductivity works against supercharging by allowing current to leak through individual grains; the balance between internal conduction and surface charging controls the maximum possible grain-to-grain electric field. Understanding the finer details of regolith grain charging, conductive equilibrium, and dielectric breakdown will improve future numerical studies of space weathering and dust levitation on airless bodies.

Effects of mixing system and pilot fuel quality on diesel-biogas dual fuel engine performance.

PubMed

Bedoya, Iván Darío; Arrieta, Andrés Amell; Cadavid, Francisco Javier

2009-12-01

This paper describes results obtained from CI engine performance running on dual fuel mode at fixed engine speed and four loads, varying the mixing system and pilot fuel quality, associated with fuel composition and cetane number. The experiments were carried out on a power generation diesel engine at 1500 m above sea level, with simulated biogas (60% CH(4)-40% CO(2)) as primary fuel, and diesel and palm oil biodiesel as pilot fuels. Dual fuel engine performance using a naturally aspirated mixing system and diesel as pilot fuel was compared with engine performance attained with a supercharged mixing system and biodiesel as pilot fuel. For all loads evaluated, was possible to achieve full diesel substitution using biogas and biodiesel as power sources. Using the supercharged mixing system combined with biodiesel as pilot fuel, thermal efficiency and substitution of pilot fuel were increased, whereas methane and carbon monoxide emissions were reduced.

Grain-Scale Supercharging and Breakdown on Airless Regoliths

NASA Technical Reports Server (NTRS)

Zimmerman, M. I.; Farrell, W. M.; Hartzell, C.M.; Wang, X.; Horanyi, M.; Hurley, D. M.; Hibbitts, K.

2016-01-01

Interactions of the solar wind and emitted photoelectrons with airless bodies have been studied extensively. However, the details of how charged particles interact with the regolith at the scale of a single grain have remained largely uncharacterized. Recent efforts have focused upon determining total surface charge under photoemission and solar wind bombardment and the associated electric field and potential. In this work, theory and simulations are used to show that grain-grain charge differences can exceed classical sheath predictions by several orders of magnitude, sometimes reaching dielectric breakdown levels. Temperature-dependent electrical conductivity works against supercharging by allowing current to leak through individual grains; the balance between internal conduction and surface charging controls the maximum possible grain-to-grain electric field. Understanding the finer details of regolith grain charging, conductive equilibrium, and dielectric breakdown will improve future numerical studies of space weathering and dust levitation on airless bodies.

Intercooler cooling-air weight flow and pressure drop for minimum drag loss

NASA Technical Reports Server (NTRS)

Reuter, J George; Valerino, Michael F

1944-01-01

An analysis has been made of the drag losses in airplane flight of cross-flow plate and tubular intercoolers to determine the cooling-air weight flow and pressure drop that give a minimum drag loss for any given cooling effectiveness and, thus, a maximum power-plant net gain due to charge-air cooling. The drag losses considered in this analysis are those due to (1) the extra drag imposed on the airplane by the weight of the intercooler, its duct, and its supports and (2) the drag sustained by the cooling air in flowing through the intercooler and its duct. The investigation covers a range of conditions of altitude, airspeed, lift-drag ratio, supercharger-pressure ratio, and supercharger adiabatic efficiency. The optimum values of cooling air pressure drop and weight flow ratio are tabulated. Curves are presented to illustrate the results of the analysis.

Supersymmetry breaking and Nambu-Goldstone fermions with cubic dispersion

NASA Astrophysics Data System (ADS)

Sannomiya, Noriaki; Katsura, Hosho; Nakayama, Yu

2017-03-01

We introduce a lattice fermion model in one spatial dimension with supersymmetry (SUSY) but without particle number conservation. The Hamiltonian is defined as the anticommutator of two nilpotent supercharges Q and Q†. Each supercharge is built solely from spinless fermion operators and depends on a parameter g . The system is strongly interacting for small g , and in the extreme limit g =0 , the number of zero-energy ground states grows exponentially with the system size. By contrast, in the large-g limit, the system is noninteracting and SUSY is broken spontaneously. We study the model for modest values of g and show that under certain conditions spontaneous SUSY breaking occurs in both finite and infinite chains. We analyze the low-energy excitations both analytically and numerically. Our analysis suggests that the Nambu-Goldstone fermions accompanying the spontaneous SUSY breaking have cubic dispersion at low energies.

A Review of Heavy-Fueled Rotary Engine Combustion Technologies

DTIC Science & Technology

2011-05-01

and Flame Quenching ...................................................................................56  4.6  Turbocharging and Supercharging... turbocharged engine). ...........................................................51  Figure 60. ISFC, exhaust temperature, power, and volumetric efficiency...OCR, CCR, and LCCR. ..............................................................61  Figure 70. Theoretical turbocharging effects on BSFC

14 CFR 145.59 - Ratings.

Code of Federal Regulations, 2010 CFR

2010-01-01

... and Space FEDERAL AVIATION ADMINISTRATION, DEPARTMENT OF TRANSPORTATION (CONTINUED) SCHOOLS AND OTHER..., cylinder head temperature gauges, or similar electrical instruments. (3) Class 3: Gyroscopic. An instrument... depends on the use of an electron tube transistor, or similar device, including supercharger, temperature...

What Protein Charging (and Supercharging) Reveal about the Mechanism of Electrospray Ionization

PubMed Central

Loo, Rachel R. Ogorzalek; Lakshmanan, Rajeswari

2014-01-01

Understanding the charging mechanism of electrospray ionization is central to overcoming shortcomings such as ion suppression or limited dynamic range and explaining phenomena such as supercharging. Towards that end, we explore what accumulated observations reveal about the mechanism of electrospray. We introduce the idea of an intermediate region for electrospray ionization (and other ionization methods) to account for the facts that solution charge state distributions (CSDs) do not correlate to those observed by ESI– MS (the latter bear more charge) and that gas phase reactions can reduce, but not increase the extent of charging. This region incorporates properties, e.g., basicities, intermediate between solution and gas phase. Assuming that droplet species polarize within the high electric field leads to equations describing ion emission resembling those from the equilibrium partitioning model. The equations predict many trends successfully, including CSD shifts to higher m/z for concentrated analytes and shifts to lower m/z for sprays employing smaller emitter opening diameters. From this view, a single mechanism can be formulated to explain how reagents that promote analyte charging (“supercharging”) such as m–NBA, sulfolane, and 3–nitrobenzonitrile increase analyte charge from “denaturing” and “native” solvent systems. It is suggested that additives’ Brønsted basicities are inversely correlated to their ability to shift CSDs to lower m/z in positive ESI, as are Brønsted acidities for negative ESI. Because supercharging agents reduce an analyte's solution ionization, excess spray charge is bestowed on evaporating ions carryingfewer opposing charges. Brønsted basicity (or acidity) determines how much ESI charge is lost to the agent (unavailable to evaporating analyte). PMID:25135609

Using Video Games to Support Pre-Service Elementary Teachers Learning of Basic Physics Principles

NASA Astrophysics Data System (ADS)

Anderson, Janice; Barnett, Michael

2011-08-01

The purpose of this work is to share our findings in using video gaming technology to facilitate the understanding of basic electromagnetism with pre-service elementary teachers. To this end we explored the impact of using a game called Supercharged! on pre-service teachers' understanding of electromagnetic concepts compared to students who conducted a more traditional inquiry oriented investigation of the same concepts. This study was a part of a larger design experiment examining the pedagogical potential of Supercharged! the control group learned through a series of guided inquiry methods while the experimental group played Supercharged! during the laboratory sections of the science course. There was significant difference F(2,134) = 4.8, p < 0.05, η2 = 0.59 between the control and experimental groups on the gains from pre-to-post assessment with an effect size of d = 0.72. However, while students in the experimental group performed better than their control group peers, they rated their knowledge of the topic lower than the control group ( M post-control = 3.0, M post-experiment = 2.7), leading to further examination of their laboratory journals. Results of this study show that video games can lead to positive learning outcomes, as demonstrated by the increase in test scores from pre- to post-assessment. Additionally, this study also suggests that a complementary approach, in which video games and hands-on activities are integrated, with each activity informing the other, could be a very powerful technique for supporting student scientific understanding. Further, our findings suggest that video game designers should embed meta-cognitive activities such as reflective opportunities into educational video games to provide scaffolds for students and to reinforce that they are engaged in an educational learning experience.

Efficient delivery of genome-editing proteins using bioreducible lipid nanoparticles

USDA-ARS?s Scientific Manuscript database

A central challenge to the development of protein-based therapeutics is the inefficiency of delivery of protein cargo across the mammalian cell membrane, including escape from endosomes. Here we report that combining bioreducible lipid nanoparticles with negatively supercharged Cre recombinase or an...

Supercharged two-cycle engines employing novel single element reciprocating shuttle inlet valve mechanisms and with a variable compression ratio

NASA Technical Reports Server (NTRS)

Wiesen, Bernard (Inventor)

2008-01-01

This invention relates to novel reciprocating shuttle inlet valves, effective with every type of two-cycle engine, from small high-speed single cylinder model engines, to large low-speed multiple cylinder engines, employing spark or compression ignition. Also permitting the elimination of out-of-phase piston arrangements to control scavenging and supercharging of opposed-piston engines. The reciprocating shuttle inlet valve (32) and its operating mechanism (34) is constructed as a single and simple uncomplicated member, in combination with the lost-motion abutments, (46) and (48), formed in a piston skirt, obviating the need for any complex mechanisms or auxiliary drives, unaffected by heat, friction, wear or inertial forces. The reciprocating shuttle inlet valve retains the simplicity and advantages of two-cycle engines, while permitting an increase in volumetric efficiency and performance, thereby increasing the range of usefulness of two-cycle engines into many areas that are now dominated by the four-cycle engine.

Pimienta-Tamabra(!) - A giant supercharged petroleum system in the southern Gulf of Mexico, onshore and offshore Mexico

USGS Publications Warehouse

Magoon, L.B.; Hudson, T.L.; Cook, H.E.

2001-01-01

Pimienta-Tamabra(!) is a giant supercharged petroleum system in the southern Gulf of Mexico with cumulative production and total reserves of 66.3 billion barrels of oil and 103.7 tcf of natural gas, or 83.6 billion barrels of oil equivalent (BOE). The effectiveness of this system results largely from the widespread distribution of good to excellent thermally mature, Upper Jurassic source rock underlying numerous stratigraphic and structural traps that contain excellent carbonate reservoirs. Expulsion of oil and gas as a supercritical fluid from Upper Jurassic source rock occurred when the thickness of overburden rock exceeded 5 km. This burial event started in the Eocene, culminated in the Miocene, and continues to a lesser extent today. The expelled hydrocarbons started migrating laterally and then upward as a gas-saturated 35-40??API oil with less than 1 wt.% sulfur and a gas-to-oil ratio (GOR) of 500-1000 ft3/BO. The generation-accumulation efficiency is about 6%.

Position-dependent mass, finite-gap systems, and supersymmetry

NASA Astrophysics Data System (ADS)

Bravo, Rafael; Plyushchay, Mikhail S.

2016-05-01

The ordering problem in quantum systems with position-dependent mass (PDM) is treated by inclusion of the classically fictitious similarity transformation into the kinetic term. This provides a generation of supersymmetry with the first-order supercharges from the kinetic term alone, while inclusion of the potential term allows us also to generate nonlinear supersymmetry with higher-order supercharges. A broad class of finite-gap systems with PDM is obtained by different reduction procedures, and general results on supersymmetry generation are applied to them. We show that elliptic finite-gap systems of Lamé and Darboux-Treibich-Verdier types can be obtained by reduction to Seiffert's spherical spiral and Bernoulli lemniscate in the presence of Calogero-like or harmonic oscillator potentials, or by angular momentum reduction of a free motion on some AdS2 -related surfaces in the presence of Aharonov-Bohm flux. The limiting cases include the Higgs and Mathews-Lakshmanan oscillator models as well as a reflectionless model with PDM exploited recently in the discussion of cosmological inflationary scenarios.

A Deconstruction Lattice Description of the D1/D5 Brane World-Volume Gauge Theory

DOE PAGES

Giedt, Joel

2011-01-01

I genermore » alize the deconstruction lattice formulation of Endres and Kaplan to two-dimensional super-QCD with eight supercharges, denoted by (4,4), and bifundamental matter. I specialize to a particularly interesting (4,4) gauge theory, with gauge group U ( N c ) × U ( N f ) , and U ( N f ) being weakly gauged. It describes the infrared limit of the D1/D5 brane system, which has been studied extensively as an example of the AdS 3 /CFT 2 correspondence. The construction here preserves two supercharges exactly and has a lattice structure quite similar to that which has previously appeared in the deconstruction approach, that is, site, link, and diagonal fields with both the Bose and Fermi statistics. I remark on possible applications of the lattice theory that would test the AdS 3 /CFT 2 correspondence, particularly one that would exploit the recent worldsheet instanton analysis of Chen and Tong.« less

Efficient delivery of genome-editing proteins using bioreducible lipid nanoparticles.

PubMed

Wang, Ming; Zuris, John A; Meng, Fantao; Rees, Holly; Sun, Shuo; Deng, Pu; Han, Yong; Gao, Xue; Pouli, Dimitra; Wu, Qi; Georgakoudi, Irene; Liu, David R; Xu, Qiaobing

2016-03-15

A central challenge to the development of protein-based therapeutics is the inefficiency of delivery of protein cargo across the mammalian cell membrane, including escape from endosomes. Here we report that combining bioreducible lipid nanoparticles with negatively supercharged Cre recombinase or anionic Cas9:single-guide (sg)RNA complexes drives the electrostatic assembly of nanoparticles that mediate potent protein delivery and genome editing. These bioreducible lipids efficiently deliver protein cargo into cells, facilitate the escape of protein from endosomes in response to the reductive intracellular environment, and direct protein to its intracellular target sites. The delivery of supercharged Cre protein and Cas9:sgRNA complexed with bioreducible lipids into cultured human cells enables gene recombination and genome editing with efficiencies greater than 70%. In addition, we demonstrate that these lipids are effective for functional protein delivery into mouse brain for gene recombination in vivo. Therefore, the integration of this bioreducible lipid platform with protein engineering has the potential to advance the therapeutic relevance of protein-based genome editing.

Quantum supercharger library: hyper-parallelism of the Hartree-Fock method.

PubMed

Fernandes, Kyle D; Renison, C Alicia; Naidoo, Kevin J

2015-07-05

We present here a set of algorithms that completely rewrites the Hartree-Fock (HF) computations common to many legacy electronic structure packages (such as GAMESS-US, GAMESS-UK, and NWChem) into a massively parallel compute scheme that takes advantage of hardware accelerators such as Graphical Processing Units (GPUs). The HF compute algorithm is core to a library of routines that we name the Quantum Supercharger Library (QSL). We briefly evaluate the QSL's performance and report that it accelerates a HF 6-31G Self-Consistent Field (SCF) computation by up to 20 times for medium sized molecules (such as a buckyball) when compared with mature Central Processing Unit algorithms available in the legacy codes in regular use by researchers. It achieves this acceleration by massive parallelization of the one- and two-electron integrals and optimization of the SCF and Direct Inversion in the Iterative Subspace routines through the use of GPU linear algebra libraries. © 2015 Wiley Periodicals, Inc. © 2015 Wiley Periodicals, Inc.

14 CFR Appendix D to Part 147 - Powerplant Curriculum Subjects

Code of Federal Regulations, 2010 CFR

2010-01-01

... (CONTINUED) SCHOOLS AND OTHER CERTIFICATED AGENCIES AVIATION MAINTENANCE TECHNICIAN SCHOOLS Pt. 147, App. D... engine temperature, pressure, and r.p.m. indicating systems. b. engine fire protection systems (3) 11... repair heat exchangers, superchargers, and turbine engine airflow and temperature control systems. (3) 28...

40 CFR 1048.125 - What maintenance instructions must I give to buyers?

Code of Federal Regulations, 2012 CFR

2012-07-01

... injectors, electronic control units, superchargers, and turbochargers: The useful life of the engine family... (CONTINUED) AIR POLLUTION CONTROLS CONTROL OF EMISSIONS FROM NEW, LARGE NONROAD SPARK-IGNITION ENGINES... and using the engine, including the emission-control system. The maintenance instructions also apply...

40 CFR 1048.125 - What maintenance instructions must I give to buyers?

Code of Federal Regulations, 2011 CFR

2011-07-01

... injectors, electronic control units, superchargers, and turbochargers: The useful life of the engine family... (CONTINUED) AIR POLLUTION CONTROLS CONTROL OF EMISSIONS FROM NEW, LARGE NONROAD SPARK-IGNITION ENGINES... and using the engine, including the emission-control system. The maintenance instructions also apply...

40 CFR 1048.125 - What maintenance instructions must I give to buyers?

Code of Federal Regulations, 2014 CFR

2014-07-01

... injectors, electronic control units, superchargers, and turbochargers: The useful life of the engine family... (CONTINUED) AIR POLLUTION CONTROLS CONTROL OF EMISSIONS FROM NEW, LARGE NONROAD SPARK-IGNITION ENGINES... and using the engine, including the emission-control system. The maintenance instructions also apply...

40 CFR 1048.125 - What maintenance instructions must I give to buyers?

Code of Federal Regulations, 2013 CFR

2013-07-01

... injectors, electronic control units, superchargers, and turbochargers: The useful life of the engine family... (CONTINUED) AIR POLLUTION CONTROLS CONTROL OF EMISSIONS FROM NEW, LARGE NONROAD SPARK-IGNITION ENGINES... and using the engine, including the emission-control system. The maintenance instructions also apply...

Fast Track to Success: Top Young Trainers 2012

ERIC Educational Resources Information Center

Freifeld, Lorri

2012-01-01

Supercharged. High-performers. Leaders of the pack. This article presents "Training" magazine's 2012 Top Young Trainers--those high-potential training professionals who are on the fast track to success. For the fifth year, "Training" magazine is pleased to recognize the outstanding talents, accomplishments, and leadership exhibited by 40 learning…

Supercharged Color: Its Arresting Place in Visual Communication.

ERIC Educational Resources Information Center

Denton, Craig L.

For centuries artists have explored the uses of color in their compositions. Believing that colors have innate symbolic, expressive, and aesthetic qualities, artists have been aware that these properties can be magnified or subdued by organization within a compositional space, and artists have suggested that certain positions within a framed field…

Pump Propels Liquid And Gas Separately

NASA Technical Reports Server (NTRS)

Harvey, Andrew; Demler, Roger

1993-01-01

Design for pump that handles mixtures of liquid and gas efficiently. Containing only one rotor, pump is combination of centrifuge, pitot pump, and blower. Applications include turbomachinery in powerplants and superchargers in automobile engines. Efficiencies lower than those achieved in separate components. Nevertheless, design is practical and results in low consumption of power.

40 CFR 1054.125 - What maintenance instructions must I give to buyers?

Code of Federal Regulations, 2011 CFR

2011-07-01

... schedule cleaning or changing air filters or changing spark plugs at the least frequent interval described... (CONTINUED) AIR POLLUTION CONTROLS CONTROL OF EMISSIONS FROM NEW, SMALL NONROAD SPARK-IGNITION ENGINES AND... aftertreatment devices, pulse-air valves, fuel injectors, oxygen sensors, electronic control units, superchargers...

40 CFR 1054.125 - What maintenance instructions must I give to buyers?

Code of Federal Regulations, 2010 CFR

2010-07-01

... schedule cleaning or changing air filters or changing spark plugs at the least frequent interval described... (CONTINUED) AIR POLLUTION CONTROLS CONTROL OF EMISSIONS FROM NEW, SMALL NONROAD SPARK-IGNITION ENGINES AND... aftertreatment devices, pulse-air valves, fuel injectors, oxygen sensors, electronic control units, superchargers...

40 CFR Appendix I to Part 94 - Emission-Related Engine Parameters and Specifications

Code of Federal Regulations, 2010 CFR

2010-07-01

... PROGRAMS (CONTINUED) CONTROL OF EMISSIONS FROM MARINE COMPRESSION-IGNITION ENGINES Pt. 94, App. I Appendix...—Reciprocating Engines. 1. Compression ratio. 2. Type of air aspiration (natural, Roots blown, supercharged.... Temperature control system calibration. 4. Maximum allowable inlet air restriction. III. Fuel System. 1...

Supercharged Snails for Stream Ecology & Water-Quality Studies

ERIC Educational Resources Information Center

Stewart, Arthur J.; Ryon, Michael G.

2003-01-01

Gill-breathing freshwater snails (Family "Pleuroceridae") are ecologically important, abundant in many streams in the United States, and easy to collect and maintain under classroom conditions. These snails can be used in classroom tests to demonstrate effects of pollutants on aquatic organisms. In more advanced classes, students can cage the…

Turnaround Momentum Still Fragile

ERIC Educational Resources Information Center

Klein, Alyson

2012-01-01

The federal program providing billions of dollars to help states and districts close or remake some of their worst-performing schools remains a work in progress after two years, with more than 1,200 turnaround efforts under way but still no definitive verdict on its effectiveness. The School Improvement Grant (SIG) program, supercharged by a…

40 CFR 1045.125 - What maintenance instructions must I give to buyers?

Code of Federal Regulations, 2014 CFR

2014-07-01

... (CONTINUED) AIR POLLUTION CONTROLS CONTROL OF EMISSIONS FROM SPARK-IGNITION PROPULSION MARINE ENGINES AND... maintaining and using the engine, including the emission control system as described in this section. The... sensors, electronic control units, superchargers, or turbochargers, except as specified in paragraph (a)(3...

14 CFR 23.1143 - Engine controls.

Code of Federal Regulations, 2014 CFR

2014-01-01

... independent of those for every other engine or supercharger. (e) For each fluid injection (other than fuel... flow of the injection fluid is adequately controlled. (f) If a power, thrust, or a fuel control (other than a mixture control) incorporates a fuel shutoff feature, the control must have a means to prevent...

14 CFR 23.1143 - Engine controls.

Code of Federal Regulations, 2013 CFR

2013-01-01

... independent of those for every other engine or supercharger. (e) For each fluid injection (other than fuel... flow of the injection fluid is adequately controlled. (f) If a power, thrust, or a fuel control (other than a mixture control) incorporates a fuel shutoff feature, the control must have a means to prevent...

14 CFR 25.1103 - Induction system ducts and air duct systems.

Code of Federal Regulations, 2013 CFR

2013-01-01

... between which relative motion could exist must have means for flexibility. (d) For turbine engine and... stage of the engine supercharger and of the auxiliary power unit compressor must have a drain to prevent... compartment to prevent hot gas reverse flow from burning through auxiliary power unit ducts and entering any...

Internal combustion engine supercharging: turbocharger vs. pressure wave compressor. Performance comparison

NASA Astrophysics Data System (ADS)

George, Atanasiu Catalin; Chiru, Anghel

2014-06-01

This paper aims on comparison between a turbocharged engine and a pressure wave charged engine. The comparison was accomplished using the engine simulation software AVL Boost, version 2010. The grahps were extracted using AVL Impress, version 2010. The performance increase is limited by the mechanical side of the simulated engine.

14 CFR 91.1069 - Flight crew: Instrument proficiency check requirements.

Code of Federal Regulations, 2013 CFR

2013-01-01

... aircraft under IFR unless, since the beginning of the 6th month before that service, that pilot has passed... command pilot of an aircraft under IFR unless, since the beginning of the 12th month before that service... engine-out speed, propeller and supercharger operations, and hydraulic, mechanical, and electrical...

14 CFR 91.1069 - Flight crew: Instrument proficiency check requirements.

Code of Federal Regulations, 2014 CFR

2014-01-01

... aircraft under IFR unless, since the beginning of the 6th month before that service, that pilot has passed... command pilot of an aircraft under IFR unless, since the beginning of the 12th month before that service... engine-out speed, propeller and supercharger operations, and hydraulic, mechanical, and electrical...

14 CFR 91.1069 - Flight crew: Instrument proficiency check requirements.

Code of Federal Regulations, 2012 CFR

2012-01-01

... aircraft under IFR unless, since the beginning of the 6th month before that service, that pilot has passed... command pilot of an aircraft under IFR unless, since the beginning of the 12th month before that service... engine-out speed, propeller and supercharger operations, and hydraulic, mechanical, and electrical...

Supercharging Lessons with a Virtual Lab

ERIC Educational Resources Information Center

Stewart, Jefferson; Vincent, Daniel

2013-01-01

The authors describes their experiences incorporating the virtual lab into a simple circuit lesson during an energy unit in a sixth-grade class. The lesson included a hands-on group experiment using wire, batteries, and light bulbs to make a circuit and an online simulation, using a virtual lab. Class discussions, student inquiries, and the study…

Learning Physics with Digital Game Simulations in Middle School Science

ERIC Educational Resources Information Center

Anderson, Janice L.; Barnett, Mike

2013-01-01

The purpose of this work is to share our findings in using video gaming technology to facilitate the understanding of basic electromagnetism with middle school students. To this end, we explored the impact of using a game called "Supercharged!" on middle school students' understanding of electromagnetic concepts compared to students…

On harmonic oscillators and their Kemmer relativistic forms

NASA Technical Reports Server (NTRS)

Debergh, Nathalie; Beckers, Jules

1993-01-01

It is shown that Dirac (Kemmer) equations are intimately connected with (para)supercharges coming from (para)supersymmetric quantum mechanics, a nonrelativistic theory. The dimensions of the irreducible representations of Clifford (Kemmer) algebras play a fundamental role in such an analysis. These considerations are illustrated through oscillator like interactions, leading to (para)relativistic oscillators.

Italian High-speed Airplane Engines

NASA Technical Reports Server (NTRS)

Bona, C F

1940-01-01

This paper presents an account of Italian high-speed engine designs. The tests were performed on the Fiat AS6 engine, and all components of that engine are discussed from cylinders to superchargers as well as the test set-up. The results of the bench tests are given along with the performance of the engines in various races.

Novel symmetries in an interacting 𝒩 = 2 supersymmetric quantum mechanical model

NASA Astrophysics Data System (ADS)

Krishna, S.; Shukla, D.; Malik, R. P.

2016-07-01

In this paper, we demonstrate the existence of a set of novel discrete symmetry transformations in the case of an interacting 𝒩 = 2 supersymmetric quantum mechanical model of a system of an electron moving on a sphere in the background of a magnetic monopole and establish its interpretation in the language of differential geometry. These discrete symmetries are, over and above, the usual three continuous symmetries of the theory which together provide the physical realizations of the de Rham cohomological operators of differential geometry. We derive the nilpotent 𝒩 = 2 SUSY transformations by exploiting our idea of supervariable approach and provide geometrical meaning to these transformations in the language of Grassmannian translational generators on a (1, 2)-dimensional supermanifold on which our 𝒩 = 2 SUSY quantum mechanical model is generalized. We express the conserved supercharges and the invariance of the Lagrangian in terms of the supervariables (obtained after the imposition of the SUSY invariant restrictions) and provide the geometrical meaning to (i) the nilpotency property of the 𝒩 = 2 supercharges, and (ii) the SUSY invariance of the Lagrangian of our 𝒩 = 2 SUSY theory.

Using Video Games to Support Pre-Service Elementary Teachers Learning of Basic Physics Principles

ERIC Educational Resources Information Center

Anderson, Janice; Barnett, Michael

2011-01-01

The purpose of this work is to share our findings in using video gaming technology to facilitate the understanding of basic electromagnetism with pre-service elementary teachers. To this end we explored the impact of using a game called "Supercharged!" on pre-service teachers' understanding of electromagnetic concepts compared to students who…

Supercharging Student Success: Policy Levers for Helping Paraprofessionals Have a Positive Influence in the Classroom. Policy Snapshot

ERIC Educational Resources Information Center

Goe, Laura; Matlach, Lauren

2014-01-01

With nearly a million paraprofessionals working in elementary and secondary schools (Bureau of Labor Statistics, 2013), ensuring they are well prepared and supported is essential to their and their students' success. Paraprofessionals work closely with classroom teachers to support students from special populations and are typically supervised by…

14 CFR 25.1093 - Induction system icing protection.

Code of Federal Regulations, 2010 CFR

2010-01-01

... using— (1) Conventional venturi carburetors have a preheater that can provide a heat rise of 120 F. with... probability of ice formation has a preheater that can provide a heat rise of 100 °F. with the engine at 60... before it enters the carburetor, the heat rise in the air caused by that supercharging at any altitude...

Supercharging Chaperones: A Meeting Toolkit for Maximizing Learning for Youth and Chaperones

ERIC Educational Resources Information Center

Brandt, Brian

2016-01-01

Trip and conference chaperones are a wonderful resource in youth development programs. These well-intended volunteers, many parents of youth participating in the event, want the best experience for the youth but are not necessarily trained in positive youth development. A consequence of this circumstance is that not all chaperones provide the best…

14 CFR Appendix C to Part 121 - C-46 Nontransport Category Airplanes

Code of Federal Regulations, 2011 CFR

2011-01-01

... Agency is one requiring the landing gear control to be placed in the up position in case of in-flight... airworthiness directives or FAA approved equivalent; and (2) Drain lines from supercharger case, engine-driven... discharge shall be such as to provide a minimum of one adequate discharge for each designated fire zone...

14 CFR Appendix C to Part 121 - C-46 Nontransport Category Airplanes

Code of Federal Regulations, 2012 CFR

2012-01-01

... Agency is one requiring the landing gear control to be placed in the up position in case of in-flight... airworthiness directives or FAA approved equivalent; and (2) Drain lines from supercharger case, engine-driven... discharge shall be such as to provide a minimum of one adequate discharge for each designated fire zone...

14 CFR Appendix C to Part 121 - C-46 Nontransport Category Airplanes

Code of Federal Regulations, 2014 CFR

2014-01-01

... Agency is one requiring the landing gear control to be placed in the up position in case of in-flight... airworthiness directives or FAA approved equivalent; and (2) Drain lines from supercharger case, engine-driven... discharge shall be such as to provide a minimum of one adequate discharge for each designated fire zone...

14 CFR Appendix C to Part 121 - C-46 Nontransport Category Airplanes

Code of Federal Regulations, 2013 CFR

2013-01-01

... Agency is one requiring the landing gear control to be placed in the up position in case of in-flight... airworthiness directives or FAA approved equivalent; and (2) Drain lines from supercharger case, engine-driven... discharge shall be such as to provide a minimum of one adequate discharge for each designated fire zone...

Improved Engine Performance and Efficiency Utilizing a Superturbocharger

DTIC Science & Technology

2012-08-01

supercharger, turbocharger and turbo-compounder in one single device. This is accomplished by mechanically controlling the speed ratio between the...the engine. This is made possible by a high efficiency turbine wheel. Normal turbochargers must balance the turbine power against the compressor...SuperTurbocharger and compare it against the currently used turbocharger in military vehicles to evaluate the impact on performance and efficiency

Supercharging Reagent for Enhanced Liquid Chromatographic Separation and Charging of Sialylated and High-Molecular-Weight Glycopeptides for NanoHPLC-ESI-MS/MS Analysis.

PubMed

Lin, Chia-Wei; Haeuptle, Micha A; Aebi, Markus

2016-09-06

Recent developments in proteomic techniques have led to the development of mass spectrometry (MS)-based methods to characterize site-specific glycosylation of proteins. However, appropriate analytical tools to characterize acidic and high-molecular-weight (hMW) glycopeptides are still lacking. In this study, we demonstrate that the addition of supercharging reagent, m-nitrobenzyl alcohol (m-NBA), into mobile phases greatly facilitates the analysis of acidic and hMW glycopeptides. Using commercial glycoproteins, we demonstrated that in the presence of m-NBA the charge state of sialylated glycopeptides increased and the chromatographic separation of neutral and acidic glycopeptides revealed a remarkable improvement. Next, we applied this system to the characterization of a glycoconjugate vaccine candidate consisting of a genetically detoxified exotoxin A of Pseudomonas aeruginosa covalently linked to Shigella flexneri type 2a O-antigen (Sf2E) produced by engineered Escherichia coli. The addition of m-NBA, allowed us to identify peptides with glycan chains of unprecedented size, up to 20 repeat units (98 monosaccharides). Our results indicated that incorporation of m-NBA into reversed-phase liquid chromatography (LC) solvents improves sensitivity, charging, and chromatographic resolution for acidic and hMW glycopeptides.

Scaling Study of Wave Rotor Turbo-normalization of a Small Internal Combustion Engine

DTIC Science & Technology

2012-09-01

14 Figure 6: Acceleration response of turbocharger versus Comprex...for increased engine performance. Turbo-normalization can be accomplished through the addition of a turbocharger , supercharger, or a pressure wave... turbocharger over the same test regime (12). The Comprex® was first used on a passenger car in 1978 on an Opel 2.1 liter diesel engine (13). In 1987

Side to Side Supercharging Allograft

DTIC Science & Technology

Side-to-side grafting between the PNA and regional in situ nerve trunks may be able to increase the effective critical length of the PNA. Nerve tissue...and provides an effective scaffolding system but depends on in situ Schwann cell migration to support axon regeneration. Though this process appears...loss and retraction can result in segmental gaps requiring some form of grafting. Autologous nerve grafting is associated with potential donor

Supersymmetric attractors, topological strings, and the M5-brane CFT

NASA Astrophysics Data System (ADS)

Guica, Monica M.

One of the purposes of this thesis is to present the consistent and unifying picture that emerges in string and M-theory with eight supercharges. On one hand, this involves classifying and relating supersymmetric objects that occur in N = 2 compactifications of string and M-theory on a Calabi-Yau manifold. These come in a surprisingly wide variety of four and five-dimensional black holes, black rings and their sometimes very complicated bound states. On the other hand, the topological string also makes its appearance in theories with eight supercharges, and turns out to compute certain black hole degeneracies. We dedicate the introduction and the first chapter to summarizing and reviewing the beautiful relationships between black holes, black rings, their dual conformal field theory and the topological string, and we also outline the remaining puzzles and issues. Some of the black holes in question can be obtained by multiply-wrapping an M-theory M5-brane on a self-intersecting four-cycle in the Calabi-Yau manifold. Their dual microscopic description is known, and consists of a two-dimensional conformal field theory (CFT) which is the low-energy limit of the gauge theory that resides on the worldvolume of the M5 brane. We show that in a certain limit the M5-brane CFT is - perhaps surprisingly - able to reproduce the entropy of a completely different type of black holes, those obtained from wrapped M2-branes, whose microscopic description has not yet been understood. We also argue that certain black hole bound states should also be described by the same CFT, which suggests a unifying description of the various black objects in eight-supercharge supergravity theories. Finally, we describe and present a proof of the so-called OSV conjecture, which states that the mixed partition function of N = 2 four-dimensional BPS black holes equals the modulus square of the type A topological string partition function. We also attempt to use this relationship to better understand corrections to the entropy of supersymmetric black holes and rings in five dimensions.

Laboratory Investigation of Ice Formation and Elimination in the Induction System of a Large Twin-engine Cargo Aircraft

NASA Technical Reports Server (NTRS)

Colis, William D

1947-01-01

The icing characteristics, the de-icing rate with hot air, and the effect of impact ice on fuel metering and mixture distribution have been determined in a laboratory investigation of that part of the engine induction system consisting of a three-barrel injection-type carburetor and a supercharger housing with spinner-type fuel injection from an 18-cylinder radial engine used on a large twin-engine cargo airplane. The induction system remained ice-free at carburetor-air temperatures above 36 F regardless of the moisture content of the air. Between carburetor-air temperatures of 32 F and 36 F with humidity ratios in excess of saturation, serious throttling ice formed in the carburetor because of expansion cooling of the air; at carburetor-air temperatures below 32 F with humidity ratios in excess of saturation, serious impact-ice formations occurred, Spinner-type fuel injection at the entrance to the supercharger and heating of the supercharger-inlet elbow and the guide vanes by the warn oil in the rear engine housing are design features that proved effective in eliminating fuel-evaporation icing and minimized the formation of throttling ice below the carburetor. Air-flow recovery time with fixed throttle was rapidly reduced as the inlet -air wet -bulb temperature was increased to 55 F; further temperature increase produced negligible improvement in recovery time. Larger ice formations and lower icing temperatures increased the time required to restore proper air flow at a given wet-bulb temperature. Impact-ice formations on the entrance screen and the top of the carburetor reduced the over-all fuel-air ratio and increased the spread between the over-all ratio and the fuel-air ratio of the individual cylinders. The normal spread of fuel-air ratio was increased from 0.020 to 0.028 when the left quarter of the entrance screen was blocked in a manner simulating the blocking resulting from ice formations released from upstream duct walls during hot-air de-icing.

The Coast Artillery Journal. Volume 72, Number 6, June 1930

DTIC Science & Technology

1930-06-01

gears between aero engine and airscrew, by the use of variable pitch airscre:vs, by engine- supercharging , by the use of stratified charges and b...atmospheric conditions are intensified until the instruments for observation are unable to penetrate and discover the target. This is very undesirable...technical expedients into Coast Artillery fire power depends on the human flux-pers()nalit~., leadership, initiative, loyalty . and teamwork. This heing

The Effect of Increased Carburetor Pressure on Engine Performance at Several Compression Ratios

NASA Technical Reports Server (NTRS)

Schey, Oscar W; Rollin, Vern G

1933-01-01

The object of this investigation was to determine the effect of increasing the carburetor pressures from 30 to 40 inches of mercury, at compression ratios from 3.5 to 7.5, on the power, on the maximum cylinder pressures, on the fuel consumption, and on the other performance characteristics of an engine. A roots-type aircraft-engine supercharger was used to maintain the desired carburetor pressure.

To Be Black, & Gifted & Red: Cold War Period Yields New, Provocative Ground for Contemporary Scholars

ERIC Educational Resources Information Center

Keels, Crystal L.

2004-01-01

Today's climate of supercharged patriotism and apparent intolerance for comment or critique calls to mind an earlier period of U.S. history. The Cold War that began in the mid-to late-1940s, along with McCarthyism and the anti-communist movement in the early 1950s, created an atmosphere of national hysteria and paranoia. For the past decade,…

Computational Science: Ensuring America’s Competitiveness

DTIC Science & Technology

2005-06-01

Supercharging U. S. Innovation & Competitiveness, Washington, D.C. , July 2004. Davies, C. T. H. , et al. , “High-Precision Lattice QCD Confronts Experiment...together to form a class of particles call hadrons (that include protons and neutrons) . For 30 years, researchers in lattice QCD have been trying to use...the basic QCD equations to calculate the properties of hadrons, especially their masses, using numerical lattice gauge theory calculations in order to

On N = 1 partition functions without R-symmetry

DOE PAGES

Knodel, Gino; Liu, James T.; Zayas, Leopoldo A. Pando

2015-03-25

Here, we examine the dependence of four-dimensional Euclidean N = 1 partition functions on coupling constants. In particular, we focus on backgrounds without R-symmetry, which arise in the rigid limit of old minimal supergravity. Backgrounds preserving a single supercharge may be classified as having either trivial or SU(2) structure, with the former including S 4. We show that, in the absence of additional symmetries, the partition function depends non-trivially on all couplings in the trivial structure case, and (anti)-holomorphically on couplings in the SU(2) structure case. In both cases, this allows for ambiguities in the form of finite counterterms, whichmore » in principle render the partition function unphysical. However, we argue that on dimensional grounds, ambiguities are restricted to finite powers in relevant couplings, and can therefore be kept under control. On the other hand, for backgrounds preserving supercharges of opposite chiralities, the partition function is completely independent of all couplings. In this case, the background admits an R-symmetry, and the partition function is physical, in agreement with the results obtained in the rigid limit of new minimal supergravity. Based on a systematic analysis of supersymmetric invariants, we also demonstrate that N = 1 localization is not possible for backgrounds without R-symmetry.« less

Method of controlling a variable geometry type turbocharger

DOE Office of Scientific and Technical Information (OSTI.GOV)

Hirabayashi, Y.

1988-08-23

This patent describes a method of controlling the supercharging pressure of a variable geometry type turbocharger having a bypass, comprising the following steps which are carried out successively: receiving signals from an engine speed sensor and from an engine knocking sensor; receiving a signal from a throttle valve sensor; judging whether or not an engine is being accelerated, and proceeding to step below if the engine is being accelerated and to step below if the engine is not being accelerated, i.e., if the engine is in a constant speed operation; determining a first correction value and proceeding to step below;more » judging whether or not the engine is knocking, and proceeding to step (d) if knocking is occurring and to step (f) below if no knocking is occurring; determining a second correction value and proceeding to step; receiving signals from the engine speed sensor and from an airflow meter which measures the quantity of airflow to be supplied to the engine; calculating an airflow rate per engine revolution; determining a duty valve according to the calculated airflow rate; transmitting the corrected duty value to control means for controlling the geometry of the variable geometry type turbocharger and the opening of bypass of the turbocharger, thereby controlling the supercharging pressure of the turbocharger.« less

A Method of Determining the Equilibrium Performance and the Stability of an Engine Equipped with an Exhaust Turbosupercharger

NASA Technical Reports Server (NTRS)

Rea, James Buchanan

1941-01-01

The performance of an exhaust turbine driving a supercharger is investigated by means of a sample calculation based on reasonable assumptions for the purpose of determining whether the assumed installation is stable with respect to changes in the mass of gas handled, boost pressure, etc. The arrangement was found to be stable throughout the entire range of operation. The method developed can be generally applied.

Performance of Blowdown Turbine driven by Exhaust Gas of Nine-Cylinder Radial Engine

DTIC Science & Technology

1944-12-01

blade speed to mean jet speed FIQUBE 6.—Variation of mean turbine efficiency with ratio of blade speed to moan Jot speed. Engine speed, 2000 rpm; full...conventional turbo - supercharger axe used in series, the blowdown turbine may be geared to the engine . Aircraft engines are operated at high speed for...guide vanes in blowdown-turblno noule box. PERFORMANCE OF BLOWDOWN TURBINE DRIVEN BT EXHAUST GAS OF RADIAL ENGINE 245 (6) Diaphragm

Composite engines for application to a single-stage-to-orbit vehicle

NASA Technical Reports Server (NTRS)

Bendot, J. G.; Brown, P. N.; Piercy, T. G.

1975-01-01

Seven composite engines were designed for application to a reusable single-stage-to-orbit vehicle. The engine designs were variations of the supercharged ejector ramjet engine. The resulting performance, weight, and drawings of each engine form a data base for establishing a potential of this class of composite engine to various missions, including the single-stage-to-orbit application. The impact of advanced technology in the design of the critical fan turbine was established.

Development of a novel passive top-down uniflow scavenged two-stroke GDI engine

DOE Office of Scientific and Technical Information (OSTI.GOV)

Ciccarelli, G.; Reynolds, Steve; Oliver, Phillip

2010-02-15

The design and performance characteristics of a novel top-down uniflow scavenged gasoline direct-injection two-stroke engine are presented. The novelty of the engine lies in the cylinder head that contains multiple check valves that control scavenging airflow into the cylinder from a supercharged air plenum. When the cylinder pressure drops below the intake plenum pressure during the expansion stroke, air flows into the cylinder through the check valves. During compression the cylinder pressure increases to a level above the intake plenum pressure and the check valves close preventing back-flow into the intake plenum. The engine head design provides asymmetrical intake valvemore » timing without the use of poppet valves and the associated valve-train. In combination with an external Roots-type supercharger that supplies the plenum and exhaust ports at the bottom of the cylinder wall, the novel head provides top-down uniflow air scavenging. Motoring tests indicated that the check valves seal and the peak pressure is governed by the compression ratio. The only drawback observed is that valve closing is delayed as the engine speed increases. In order to investigate the valve dynamics, additional tests were performed in an optically-accessible cold flow test rig that enabled the direct measurement of valve opening and closing time under various conditions. (author)« less

The effect of charge mutations on the stability and aggregation of a human single chain Fv fragment.

PubMed

Austerberry, James I; Dajani, Rana; Panova, Stanislava; Roberts, Dorota; Golovanov, Alexander P; Pluen, Alain; van der Walle, Christopher F; Uddin, Shahid; Warwicker, Jim; Derrick, Jeremy P; Curtis, Robin

2017-06-01

The aggregation propensities for a series of single-chain variable fragment (scFv) mutant proteins containing supercharged sequences, salt bridges and lysine/arginine-enriched motifs were characterised as a function of pH and ionic strength to isolate the electrostatic contributions. Recent improvements in aggregation predictors rely on using knowledge of native-state protein-protein interactions. Consistent with previous findings, electrostatic contributions to native protein-protein interactions correlate with aggregate growth pathway and rates. However, strong reversible self-association observed for selected mutants under native conditions did not correlate with aggregate growth, indicating 'sticky' surfaces that are exposed in the native monomeric state are inaccessible when aggregates grow. We find that even though similar native-state protein-protein interactions occur for the arginine and lysine-enriched mutants, aggregation propensity is increased for the former and decreased for the latter, providing evidence that lysine suppresses interactions between partially folded states under these conditions. The supercharged mutants follow the behaviour observed for basic proteins under acidic conditions; where excess net charge decreases conformational stability and increases nucleation rates, but conversely reduces aggregate growth rates due to increased intermolecular electrostatic repulsion. The results highlight the limitations of using conformational stability and native-state protein-protein interactions as predictors for aggregation propensity and provide guidance on how to engineer stabilizing charged mutations. Copyright © 2017. Published by Elsevier B.V.

Supercharging with Trivalent Metal Ions in Native Mass Spectrometry

PubMed Central

Flick, Tawnya G.; Williams, Evan R.

2012-01-01

Addition of 1.0 mM LaCl3 to aqueous ammonium acetate solutions containing proteins in their folded native forms can result in a significant increase in the molecular ion charging obtained with electrospray ionization as a result of cation adduction. In combination with m-nitrobenzyl alcohol, molecular ion charge states that are greater than the number of basic sites in the protein can be produced from these native solutions, even for lysozyme, which is conformationally constrained by four intramolecular disulfide bonds. Circular dichroism spectroscopy indicates that the conformation of ubiquitin is not measurably affected with up to 1.0 M LaCl3, but ion mobility data indicate that the high charge states that are formed when 1.0 mM LaCl3 is present are more unfolded than the low charge states formed without this reagent. These and other results indicate that the increased charging is a result of La3+ preferentially adducting onto compact or more native-like conformers during ESI and the gas-phase ions subsequently unfolding as a result of increased Coulomb repulsion. Electron capture dissociation of these high charge-state ions formed from these native solutions results in comparable sequence coverage to that obtained for ions formed from denaturing solutions without supercharging reagents, making this method a potentially powerful tool for obtaining structural information in native mass spectrometry. PMID:22948901

Design and Simulation of a Pressure Wave Supercharger for a Small Two-Stroke Engine

DTIC Science & Technology

2014-03-27

Air at ambient pressure is passed through the compressor where the pressure is increased with the intended purpose of increasing the overall mass flow...rate of air to the intake manifold. For a small two-stroke engine that has little excess energy to spare for the operation of a compressor , the...exhaust gasses from the engine to drive a turbine that is linked via a shaft to a centrifugal compressor which feeds compressed air to the intake

Chiral algebras in Landau-Ginzburg models

NASA Astrophysics Data System (ADS)

Dedushenko, Mykola

2018-03-01

Chiral algebras in the cohomology of the {\\overline{Q}}+ supercharge of two-dimensional N=(0,2) theories on flat spacetime are discussed. Using the supercurrent multiplet, we show that the answer is renormalization group invariant for theories with an R-symmetry. For N=(0,2) Landau-Ginzburg models, the chiral algebra is determined by the operator equations of motion, which preserve their classical form, and quantum renormalization of composite operators. We study these theories and then specialize to the N=(2,2) models and consider some examples.

Superalgebras for three interacting particles in an external magnetic field

NASA Astrophysics Data System (ADS)

Sadeghi, J.

2006-04-01

In this paper we discuss interacting particles in an external magnetic field. By comparing the Schrödinger equation of three interacting particles with the associated Laguerre differential equation, we obtain the energy spectrum which corresponds to indices ni and mi. Finally by using the so called factorization method we obtain the raising and lowering operators. These operators are supersymmetric structures related to the Hamiltonian partner. Also these operators lead to the realization of Heisenberg Lie superalgebras with two, four and six supercharges.

Two-Stage Supercharging

DTIC Science & Technology

1941-02-01

Lnterstage Valves are open. Under these conditions the pressure at the carbu- ..retor entrance-will be governed . by atmo~pherlc conditions...he exce~tidnt hat the control is” r’eepomsive ,,to and governs the:~resaufi6 after- the carbu- retor inst gad of %efor.~ it. ““ “’ -. ). From the...highl-y, .,sup.&rGhar&ed,... ... .. . . In th”e 10 XACA ,1’ethnic.al Note lNo O.7$4 . follow lng~ c.ontrule a“re’nec.essary, .t.o govern and .lirni.t

Supersymmetric Casimir energy and the anomaly polynomial

NASA Astrophysics Data System (ADS)

Bobev, Nikolay; Bullimore, Mathew; Kim, Hee-Cheol

2015-09-01

We conjecture that for superconformal field theories in even dimensions, the supersymmetric Casimir energy on a space with topology S 1 × S D-1 is equal to an equivariant integral of the anomaly polynomial. The equivariant integration is defined with respect to the Cartan subalgebra of the global symmetry algebra that commutes with a given supercharge. We test our proposal extensively by computing the supersymmetric Casimir energy for large classes of superconformal field theories, with and without known Lagrangian descriptions, in two, four and six dimensions.

G-structures and domain walls in heterotic theories

NASA Astrophysics Data System (ADS)

Lukas, Andre; Matti, Cyril

2011-01-01

We consider heterotic string solutions based on a warped product of a four-dimensional domain wall and a six-dimensional internal manifold, preserving two supercharges. The constraints on the internal manifolds with SU(3) structure are derived. They are found to be generalized half-flat manifolds with a particular pattern of torsion classes and they include half-flat manifolds and Strominger's complex non-Kahler manifolds as special cases. We also verify that previous heterotic compactifications on half-flat mirror manifolds are based on this class of solutions.

Surface charge- and space-dependent transport of proteins in crowded environments of nanotailored posts.

PubMed

Choi, Chang Kyoung; Fowlkes, Jason D; Retterer, Scott T; Siuti, Piro; Iyer, Sukanya; Doktycz, Mitchel J

2010-06-22

The reaction and diffusion of molecules across barriers and through crowded environments is integral to biological system function and to separation technologies. Ordered, microfabricated post arrays are a promising route to creating synthetic barriers with controlled chemical and physical characteristics. They can be used to create crowded environments, to mimic aspects of cellular membranes, and to serve as engineered replacements of polymer-based separation media. Here, the translational diffusion of fluorescein isothiocyante and various forms of green fluorescent protein (GFP), including "supercharged" variants, are examined in a silicon-based post array environment. The technique of fluorescence recovery after photobleaching (FRAP) is combined with analytical approximations and numerical simulations to assess the relative effects of reaction and diffusion on molecular transport, respectively. FRAP experiments were conducted for 64 different cases where the molecular species, the density of the posts, and the chemical surface charge of the posts were varied. In all cases, the dense packing of the posts hindered the diffusive transport of the fluorescent species. The supercharged GFPs strongly interacted with oppositely charged surfaces. With similar molecular and surface charges, transport is primarily limited by hindered diffusion. For conventional, enhanced GFP in a positively charged surface environment, transport was limited by the coupled action of hindered diffusion and surface interaction with the posts. Quantification of the size-, space-, time-, and charge-dependent translational diffusion in the post array environments can provide insight into natural processes and guide the design and development of selective membrane systems.

Supercharging of the Lunar Surface by Solar Wind Halo Electrons

NASA Astrophysics Data System (ADS)

Stubbs, T. J.; Farrell, W. M.; Collier, M. R.; Halekas, J. S.; Delory, G. T.; Holland, M. P.; Vondrak, R. R.

2007-12-01

Lunar surface potentials can reach several kilovolts negative during Solar Energetic Particle (SEPs) events, as indicated by recent analysis of data from the Lunar Prospector Electron Reflectometer (LP/ER). The lunar surface- plasma interactions that result in such extreme surface potentials are poorly characterized and understood. Extreme lunar surface charging, and the associated electrostatic discharges and transport of charged dust, will likely present significant hazards to future human explorers. This is of particular concern near the terminator and polar regions, such as the South Pole/Aiken Basin site planned for NASA's manned outpost. It is the flux of electrons from the ambient plasma that charges the surface of the Moon to negative potentials. In the solar wind, the electron temperature is typically ~10 eV which tends to charge the lunar surface to ~100 V negative in shadow. However, during space weather events the solar wind electrons are often better described by the sum of two Maxwellian distributions, referred to as the "core" and "halo" components. The core electrons are relatively cool and dense (e.g., ~10 eV and ~10/cc), whereas the halo electrons are hot and tenuous (e.g., ~100 eV and ~0.1/cc). Despite, the tenuous nature of the halo electrons, our surface charging model - using core and halo electron data derived from the Solar Wind Experiment (SWE) aboard the Wind spacrcraft - predicts that they are capable of "supercharging" the lunar surface to kilovolt potentials during space weather events, which could explain the LP/ER observations.

Photoelectric charging of partially sunlit dielectric surfaces in space

NASA Technical Reports Server (NTRS)

De, B. R.; Criswell, D. R.

1977-01-01

Sunlight-shadow effects may substantially alter the charging situation for a dielectric surface. The sunlight-shadow boundary tends to be the site of intense multipole electric fields. Charges on a sunlit dielectric surface have a finite effective mobility. The charge distribution tends to resemble that on a conducting surface. A boundary between a conducting and a dielectric surface may not represent a conductivity discontinuity when this boundary is sunlit; charges may migrate at a nontrivial rate across the boundary. A contracting or expanding sunlit area may experience a supercharging.

Ignition and combustion: Low compression ratio, high output diesel

NASA Technical Reports Server (NTRS)

1981-01-01

The feasibility of converting a spark ignition aircraft engine GTSI0-520 to compression ignition without increasing the peak combustion pressure of 1100 lbs/sq.in. was determined. The final contemplated utilized intake air heating at idle and light load and a compression ratio of about 10:1 with a small amount of fumigation (the addition of about 15% fuel into the combustion air before the cylinder). The engine used was a modification of a Continental-Teledyne gasoline engine cylinder from the GTSI0-520 supercharged aircraft engine.

Electrokinetic supercharging with a system-induced terminator and an optimized capillary versus electrode configuration for parts-per-trillion detection of rare-earth elements in CZE.

PubMed

Xu, Zhongqi; Kawahito, Kouji; Ye, Xiaoxue; Timerbaev, Andrei R; Hirokawa, Takeshi

2011-05-01

A further improvement of electrokinetic supercharging (EKS) methodology has been proposed, with the objective to enhance the sensitivity of the conventional CZE-UV method down to a single-digit part per trillion (ppt) level. The advanced EKS procedure is based on a novel phenomenon displaying the formation of a zone with an increased concentration of the hydrogen ion, capable to perform the function of a terminator, behind the sample zone upon electrokinetic injection. In combination with a visualizing co-ion of BGE, protonated 4-methylbenzylamine, acting as the leading ion, such system-induced terminator a effected the transient ITP state to efficiently concentrate cationic analytes prior to CZE. Furthermore, to amass more analyte ions within the effective electric field at the injection stage, a standard sample vial was replaced with an elongated vial that allowed the sample volume to be increased from 500 to 900 μL. Alongside, this replacement made the upright distance between the electrode and the capillary tips prolonged to 40.0 mm to achieve high-efficiency electrokinetic injection. The computer simulation was used for profiling analyte concentration, pH, and field strength in order to delineate formation of the terminator during sample injection. The proposed preconcentration strategy afforded an enrichment factor of 80,000 and thereby the LODs of rare-earth metal ions at the ppt level, e.g. 0.04 nM (6.7 ng/L) for erbium(III). Copyright © 2011 WILEY-VCH Verlag GmbH & Co. KGaA, Weinheim.

Supercharged end-to-side anterior interosseous to ulnar motor nerve transfer for intrinsic musculature reinnervation.

PubMed

Barbour, John; Yee, Andrew; Kahn, Lorna C; Mackinnon, Susan E

2012-10-01

Functional motor recovery after peripheral nerve injury is predominantly determined by the time to motor end plate reinnervation and the absolute number of regenerated motor axons that reach target. Experimental models have shown that axonal regeneration occurs across a supercharged end-to-side (SETS) nerve coaptation. In patients with a recovering proximal ulnar nerve injury, a SETS nerve transfer conceptually is useful to protect and preserve distal motor end plates until the native axons fully regenerate. In addition, for nerve injuries in which incomplete regeneration is anticipated, a SETS nerve transfer may be useful to augment the regenerating nerve with additional axons and to more quickly reinnervate target muscle. We describe our technique for a SETS nerve transfer of the terminal anterior interosseous nerve (AIN) to the pronator quadratus muscle (PQ) end-to-side to the deep motor fascicle of the ulnar nerve in the distal forearm. In addition, we describe our postoperative therapy regimen for these transfers and an evaluation tool for monitoring progressive muscle reinnervation. Although the AIN-to-ulnar motor group SETS nerve transfer was specifically designed for ulnar nerve injuries, we believe that the SETS procedure might have broad clinical utility for second- and third-degree axonotmetic nerve injuries, to augment partial recovery and/or "babysit" motor end plates until the native parent axons regenerate to target. We would consider all donor nerves currently utilized in end-to-end nerve transfers for neurotmetic injuries as candidates for this SETS technique. Copyright © 2012 American Society for Surgery of the Hand. Published by Elsevier Inc. All rights reserved.

Integration of electrochemistry with ultra-performance liquid chromatography/mass spectrometry.

PubMed

Cai, Yi; Zheng, Qiuling; Liu, Yong; Helmy, Roy; Loo, Joseph A; Chen, Hao

2015-01-01

This study presents the development of ultra-performance liquid chromatography (UPLC) mass spectrometry (MS) combined with electrochemistry (EC) for the first time and its application for the structural analysis of proteins/peptides that contain disulfide bonds. In our approach, a protein/peptide mixture sample undergoes a fast UPLC separation and subsequent electrochemical reduction in an electrochemical flow cell followed by online MS and tandem mass spectrometry (MS/MS) analyses. The electrochemical cell is coupled to the mass spectrometer using our recently developed desorption electrospray ionization (DESI) interface. Using this UPLC/EC/DESI-MS method, peptides that contain disulfide bonds can be differentiated from those without disulfide bonds, as the former are electroactive and reducible. MS/MS analysis of the disulfide-reduced peptide ions provides increased information on the sequence and disulfide-linkage pattern. In a reactive DESI- MS detection experiment in which a supercharging reagent was used to dope the DESI spray solvent, increased charging was obtained for the UPLC-separated proteins. Strikingly, upon online electrolytic reduction, supercharged proteins (e.g., α-lactalbumin) showed even higher charging, which will be useful in top- down protein structure MS analysis as increased charges are known to promote protein ion dissociation. Also, the separation speed and sensitivity are enhanced by approximately 1(~)2 orders of magnitude by using UPLC for the liquid chromatography (LC)/EC/MS platform, in comparison to the previously used high- performance liquid chromatography (HPLC). This UPLC/EC/DESI-MS method combines the power of fast UPLC separation, fast electrochemical conversion, and online MS structural analysis for a potentially valuable tool for proteomics research and bioanalysis.

Integration of Electrochemistry with Ultra Performance Liquid Chromatography/Mass Spectrometry (UPLC/MS)

PubMed Central

Cai, Yi; Zheng, Qiuling; Liu, Yong; Helmy, Roy; Loo, Joseph A.; Chen, Hao

2015-01-01

This study presents the development of ultra-performance liquid chromatography/mass spectrometry (UPLC/MS) combined with electrochemistry (EC) for the first time and its application for the structural analysis of disulfide bond-containing proteins/peptides. In our approach, a protein/peptide mixture sample undergoes fast UPLC separation and subsequent electrochemical reduction in an electrochemical flow cell followed by online MS and MS/MS analyses. The electrochemical cell is coupled to MS using our recently developed desorption electrospray ionization (DESI) interface. Using this UPLC/EC/DESI-MS method, disulfide bond-containing peptides can be differentiated from those without disulfide bonds as the former are electroactive and reducible. Tandem MS analysis of the disulfide-reduced peptide ions provides increased sequence and disulfide linkage pattern information. In a reactive DESI-MS detection experiment in which a supercharging reagent was used to dope the DESI spray solvent, increased charging was obtained for the UPLC-separated proteins. Strikingly, upon online electrolytic reduction, supercharged proteins (e.g., α-lactalbumin) showed even higher charging, which would be useful in top-down protein structure analysis as increased charges are known to promote protein ion dissociation. Also, the separation speed and sensitivity are enhanced by approximately 1~2 orders of magnitude by using UPLC for the LC/EC/MS platform, in comparison to the previously used high performance liquid chromatography (HPLC). This UPLC/EC/DESI-MS method combines the power of fast UPLC separation, fast electrochemical conversion and online MS structural analysis for a potentially valuable tool for proteomics research and bioanalysis. PMID:26307715

Goedel, Penrose, anti-Mach: Extra supersymmetries of time-dependent plane waves

NASA Astrophysics Data System (ADS)

Blau, Matthias; Meessen, Patrick; O'Loughlin, Martin

2003-09-01

We prove that M-theory plane waves with extra supersymmetries are necessarily homogeneous (but possibly time-dependent), and we show by explicit construction that such time-dependent plane waves can admit extra supersymmetries. To that end we study the Penrose limits of Gödel-like metrics, show that the Penrose limit of the M-theory Gödel metric (with 20 supercharges) is generically a time-dependent homogeneous plane wave of the anti-Mach type, and display the four extra Killings spinors in that case. We conclude with some general remarks on the Killing spinor equations for homogeneous plane waves.

Efficient in vitro encapsulation of protein cargo by an engineered protein container.

PubMed

Wörsdörfer, Bigna; Pianowski, Zbigniew; Hilvert, Donald

2012-01-18

An engineered variant of lumazine synthase, a nonviral capsid protein with a negatively charged luminal surface, is shown to encapsulate up to 100 positively supercharged green fluorescent protein (GFP) molecules in vitro. Packaging can be achieved starting either from intact, empty capsids or from capsid fragments by incubation with cargo in aqueous buffer. The yield of encapsulated GFP correlates directly with the host/guest mixing ratio, providing excellent control over packing density. Facile in vitro loading highlights the unusual structural dynamics of this novel nanocontainer and should facilitate diverse biotechnological and materials science applications. © 2011 American Chemical Society

Approche Kaluza-Klein et Supersymetrie de Jauge

NASA Astrophysics Data System (ADS)

Pare, Jean-Pierre

This thesis presents a non-Abelian gauge-supersymmetric Kaluza-Klein approach for charged spinning particles and strings in a background of gravitational and Yang-Mills fields. In the classical Kaluza-Klein approach, the basic mathematical structure is a principal bundle of which the base manifold is space-time. This principal bundle is endowed with a pseudo-Riemannian metric, invariant under the action of the structural group of the bundle, and a connection. Geodesic equations on the bundle lead to the Maxwell-Lorentz equation for curved space-time and Yang -Mills fields, and to a conservation law of a non-Abelian (bosonic) charge. This conservation law originates from the invariance of the free-particle action on the bundle under the action of the structural group of the bundle (gauge group). Firstly, we generalize this approach for a spinning particle. The spin of the particle is described by Grassmannian variables added to the principal bundle. This supersymmetrization gives rise, in addition to the bosonic non-Abelian charge, a fermionic one. This leads to a search for a supergroup action on the superprincipal bundle which leaves invariant the action of the spinning particle. The invariance of this action would lead to the conservation of a non-Abelian super-charge, generalizing the conservation law obtained for particles without spin. We present Lagrangian and Hamiltonian formulations, both invariant under a super -group action. The equations of motion are derived and discussed. Different terms in these equations are well known in the literature. The invariance of these formulations under a supergroup action leads to a conservation law of a non-Abelian supercharge. The bosonic part of this supercharge corresponds to the non-Abelian (bosonic) charge obtained for a particle without spin. The fermionic part is a non -physical charge. It turns out in the supersymmetric case that this decouples from all other dynamical variables, and hence it does not influence trajectories of spinning particles. It is interesting to mention how this gauge -supersymmetry is introduced in the dynamics. It arises by choosing the unique metric connection on the principal bundle with torsion given by the Chern-Simons 3-form. We then proceed to extend these formulations for spinning strings. We present Lagrangian and Hamiltonian gauge-supersymmetric formulations in a superloop space setting. The same connection corresponding to the Chern -Simons 3-form is used here. Equations of motion are derived and discussed. In the appendix, we discuss the effect of using this connection in a non-Abelian Kaluza-Klein field theory. Using the same connection, we present a non-Abelian Kaluza-Klein approach leading to a zero cosmological constant.

A New, Highly Improved Two-Cycle Engine

NASA Technical Reports Server (NTRS)

Wiesen, Bernard

2008-01-01

The figure presents a cross-sectional view of a supercharged, variable-compression, two-cycle, internal-combustion engine that offers significant advantages over prior such engines. The improvements are embodied in a combination of design changes that contribute synergistically to improvements in performance and economy. Although the combination of design changes and the principles underlying them are complex, one of the main effects of the changes on the overall engine design is reduced (relative to prior two-cycle designs) mechanical complexity, which translates directly to reduced manufacturing cost and increased reliability. Other benefits include increases in the efficiency of both scavenging and supercharging. The improvements retain the simplicity and other advantages of two-cycle engines while affording increases in volumetric efficiency and performance across a wide range of operating conditions that, heretofore have been accessible to four-cycle engines but not to conventionally scavenged two-cycle ones, thereby increasing the range of usefulness of the two-cycle engine into all areas now dominated by the four-cycle engine. The design changes and benefits are too numerous to describe here in detail, but it is possible to summarize the major improvements: Reciprocating Shuttle Inlet Valve The entire reciprocating shuttle inlet valve and its operating gear is constructed as a single member. The shuttle valve is actuated in a lost-motion arrangement in which, at the ends of its stroke, projections on the shuttle valve come to rest against abutments at the ends of grooves in a piston skirt. This shuttle-valve design obviates the customary complex valve mechanism, actuated from an engine crankshaft or camshaft, yet it is effective with every type of two-cycle engine, from small high-speed single cylinder model engines, to large low-speed multiple cylinder engines.

A lower isoelectric point increases signal sequence-mediated secretion of recombinant proteins through a bacterial ABC transporter.

PubMed

Byun, Hyunjong; Park, Jiyeon; Kim, Sun Chang; Ahn, Jung Hoon

2017-12-01

Efficient protein production for industrial and academic purposes often involves engineering microorganisms to produce and secrete target proteins into the culture. Pseudomonas fluorescens has a TliDEF ATP-binding cassette transporter, a type I secretion system, which recognizes C-terminal LARD3 signal sequence of thermostable lipase TliA. Many proteins are secreted by TliDEF in vivo when recombined with LARD3, but there are still others that cannot be secreted by TliDEF even when LARD3 is attached. However, the factors that determine whether or not a recombinant protein can be secreted through TliDEF are still unknown. Here, we recombined LARD3 with several proteins and examined their secretion through TliDEF. We found that the proteins secreted via LARD3 are highly negatively charged with highly-acidic isoelectric points (pI) lower than 5.5. Attaching oligo-aspartate to lower the pI of negatively-charged recombinant proteins improved their secretion, and attaching oligo-arginine to negatively-charged proteins blocked their secretion by LARD3. In addition, negatively supercharged green fluorescent protein (GFP) showed improved secretion, whereas positively supercharged GFP did not secrete. These results disclosed that proteins' acidic pI and net negative charge are major factors that determine their secretion through TliDEF. Homology modeling for TliDEF revealed that TliD dimer forms evolutionarily-conserved positively-charged clusters in its pore and substrate entrance site, which also partially explains the pI dependence of the TliDEF-dependent secretions. In conclusion, lowering the isoelectric point improved LARD3-mediated protein secretion, both widening the range of protein targets for efficient production via secretion and signifying an important aspect of ABC transporter-mediated secretions. © 2017 by The American Society for Biochemistry and Molecular Biology, Inc.

Band-broadening suppressed effect in long turned geometry channel and high-sensitive analysis of DNA sample by using floating electrokinetic supercharging on a microchip.

PubMed

Xu, Zhongqi; Murata, Kenji; Arai, Akihiro; Hirokawa, Takeshi

2010-03-12

A featured microchip owning three big reservoirs and long turned geometry channel was designed to improve the detection limit of DNA fragments by using floating electrokinetic supercharging (FEKS) method. The novel design matches the FEKS preconcentration needs of a large sample volume introduction with electrokinetic injection (EKI), as well as long duration of isotachophoresis (ITP) process to enrich low concentration sample. In the curved channel [ approximately 45.6 mm long between port 1 (P1) and the intersection point of two channels], EKI and ITP were performed while the side port 3 (P3) was electrically floated. The turn-induced band broadening with or without ITP process was investigated by a computer simulation (using CFD-ACE+ software) when the analytes traveling through the U-shaped geometry. It was found that the channel curvature determined the extent of band broadening, however, which could be effectively eliminated by the way of ITP. After the ITP-stacked zones passed the intersection point from P1, they were rapidly destacked for separation and detection from ITP to zone electrophoresis by using leading ions from P3. The FEKS carried on the novel chip successfully contributed to higher sensitivities of DNA fragments in comparison with our previous results realized on either a single channel or a cross microchip. The analysis of low concentration 50 bp DNA step ladders (0.23 mugml after 1500-fold diluted) was achieved with normal UV detection at 260 nm. The obtained limit of detections (LODs) were on average 100 times better than using conventional pinched injection, down to several ngml for individual DNA fragment.

Modeling the complete Otto cycle: Preliminary version. [computer programming

NASA Technical Reports Server (NTRS)

Zeleznik, F. J.; Mcbride, B. J.

1977-01-01

A description is given of the equations and the computer program being developed to model the complete Otto cycle. The program incorporates such important features as: (1) heat transfer, (2) finite combustion rates, (3) complete chemical kinetics in the burned gas, (4) exhaust gas recirculation, and (5) manifold vacuum or supercharging. Changes in thermodynamic, kinetic and transport data as well as model parameters can be made without reprogramming. Preliminary calculations indicate that: (1) chemistry and heat transfer significantly affect composition and performance, (2) there seems to be a strong interaction among model parameters, and (3) a number of cycles must be calculated in order to obtain steady-state conditions.

Effect of the NACA Injection Impeller on the Mixture Distribution of a Double-row Radial Aircraft Engine

NASA Technical Reports Server (NTRS)

Marble, Frank E.; Ritter, William K.; Miller, Mahlon A.

1946-01-01

For the normal range of engine power the impeller provided marked improvement over the standard spray-bar injection system. Mixture distribution at cruising was excellent, maximum cylinder temperatures were reduced about 30 degrees F, and general temperature distribution was improved. The uniform mixture distribution restored the normal response of cylinder temperature to mixture enrichment and it reduced the possibility of carburetor icing, while no serious loss in supercharger pressure rise resulted from injection of fuel near the impeller outlet. The injection impeller also furnished a convenient means of adding water to the charge mixture for internal cooling.

Practical Possibilities of High-Altitude Flight with Exhaust-Gas Turbines in Connection with Spark Ignition Engines Comparative Thermodynamic and Flight Mechanical Investigations

NASA Technical Reports Server (NTRS)

Weise, A.

1947-01-01

As a means of preparing for high-altitude flight with spark-ignition engines in conjunction with exhaust-gas turbosuperchargers, various methods of modifying the exhaust-gas temperatures, which are initially higher than a turbine can withstand are mathematically compared. The thermodynamic results first obtained are then examined with respect to the effect on flight speed, climbing speed, ceiling, economy, and cruising range. The results are so presented in a generalized form that they may be applied to every appropriate type of aircraft design and a comparison with the supercharged engine without exhaust-gas turbine can be made.

Airbreathing combined cycle engine systems

NASA Technical Reports Server (NTRS)

Rohde, John

1992-01-01

The Air Force and NASA share a common interest in developing advanced propulsion systems for commercial and military aerospace vehicles which require efficient acceleration and cruise operation in the Mach 4 to 6 flight regime. The principle engine of interest is the turboramjet; however, other combined cycles such as the turboscramjet, air turborocket, supercharged ejector ramjet, ejector ramjet, and air liquefaction based propulsion are also of interest. Over the past months careful planning and program implementation have resulted in a number of development efforts that will lead to a broad technology base for those combined cycle propulsion systems. Individual development programs are underway in thermal management, controls materials, endothermic hydrocarbon fuels, air intake systems, nozzle exhaust systems, gas turbines and ramjet ramburners.

Advanced automotive diesel engine system study

NASA Technical Reports Server (NTRS)

1983-01-01

A conceptual study of an advanced automotive diesel engine is discussed. The engine concept selected for vehicle installation was a supercharged 1.4 liter, 4 cylinder spark assisted diesel of 14:1 compression ratio. A compounding unit consisting of a Lysholm compressor and expander is connected to the engine crankshaft by a belt drive. The inlet air charge is heated by the expander exhaust gas via a heat exchanger. Four levels of technology achievement on the selected engine concept were evaluated, from state-of-the-art to the ideal case. This resulted in the fuel economy increasing from 53.2 mpg to 81.7 mpg, and the 0-60 mph time decreasing from 17.6 seconds to 10.9 seconds.

Implementing Photodissociation in an Orbitrap Mass Spectrometer

PubMed Central

Vasicek, Lisa A.; Ledvina, Aaron R.; Shaw, Jared; Griep-Raming, Jens; Westphall, Michael S.; Coon, Joshua J.; Brodbelt, Jennifer S.

2011-01-01

We modified a dual pressure linear ion trap Orbitrap to permit infrared multiphoton dissociation (IRMPD) in the higher energy collisional dissociation (HCD) cell for high resolution analysis. A number of parameters, including the pressures of the C-trap and HCD cell, the radio frequency (rf) amplitude applied to the C-trap, and the HCD DC offset, were evaluated to optimize IRMPD efficiency and maintain a high signal-to-noise ratio. IRMPD was utilized for characterization of phosphopeptides, supercharged peptides, and N-terminal modified peptides, as well as for top-down protein analysis. The high resolution and high mass accuracy capabilities of the Orbitrap analyzer facilitated confident assignment of product ions arising from IRMPD. PMID:21953052

Performance of NACA Eight-stage Axial-flow Compressor Designed on the Basis of Airfoil Theory

NASA Technical Reports Server (NTRS)

Sinnette, John T; Schey, Oscar W; King, J Austin

1943-01-01

The NACA has conducted an investigation to determine the performance that can be obtained from a multistage axial-flow compressor based on airfoil research. A theory was developed; an eight-stage axial-flow compressor was designed, constructed, and tested. The performance of the compressor was determined for speeds from 5000 to 14,000 r.p.m with varying air flow at each speed. Most of the tests were made with air at room temperature. The performance was determined in accordance with the Committee's recommended procedure for testing superchargers. The expected performance was obtained, showing that a multistage compressor of high efficiency can be designed by the application of airfoil theory.

Roots Air Management System with Integrated Expander

DOE Office of Scientific and Technical Information (OSTI.GOV)

Stretch, Dale; Wright, Brad; Fortini, Matt

2016-07-06

PEM fuel cells remain an emerging technology in the vehicle market with several cost and reliability challenges that must be overcome in order to increase market penetration and acceptance. The DOE has identified the lack of a cost effective, reliable, and efficient air supply system that meets the operational requirements of a pressurized PEM 80kW fuel cell as one of the major technological barriers that must be overcome. This project leveraged Roots positive displacement development advancements and demonstrated an efficient and low cost fuel cell air management system. Eaton built upon its P-Series Roots positive displacement design and shifted themore » peak efficiency making it ideal for use on an 80kW PEM stack. Advantages to this solution include: • Lower speed of the Roots device eliminates complex air bearings present on other systems. • Broad efficiency map of Roots based systems provides an overall higher drive cycle fuel economy. • Core Roots technology has been developed and validated for other transportation applications. Eaton modified their novel R340 Twin Vortices Series (TVS) Roots-type supercharger for this application. The TVS delivers more power and better fuel economy in a smaller package as compared to other supercharger technologies. By properly matching the helix angle with the rotor’s physical aspect ratio, the supercharger’s peak efficiency can be moved to the operating range where it is most beneficial for the application. The compressor was designed to meet the 90 g/s flow at a pressure ratio of 2.5, similar in design to the P-Series 340. A net shape plastic expander housing with integrated motor and compressor was developed to significantly reduce the cost of the system. This integrated design reduced part count by incorporating an overhung expander and motor rotors into the design such that only four bearings and two shafts were utilized.« less

Super-BMS3 algebras from {N}=2 flat supergravities

NASA Astrophysics Data System (ADS)

Lodato, Ivano; Merbis, Wout

2016-11-01

We consider two possible flat space limits of three dimensional {N}=(1, 1) AdS supergravity. They differ by how the supercharges are scaled with the AdS radius ℓ: the first limit (democratic) leads to the usual super-Poincaré theory, while a novel `twisted' theory of supergravity stems from the second (despotic) limit. We then propose boundary conditions such that the asymptotic symmetry algebras at null infinity correspond to supersymmetric extensions of the BMS algebras previously derived in connection to non- and ultra-relativistic limits of the {N}=(1, 1) Virasoro algebra in two dimensions. Finally, we study the supersymmetric energy bounds and find the explicit form of the asymptotic and global Killing spinors of supersymmetric solutions in both flat space supergravity theories.

Total cost of 46-Mw Borax cogen system put at $30M

DOE Office of Scientific and Technical Information (OSTI.GOV)

de Biasi, V.

1983-03-01

The cogeneration system, designed around a W-251B gas turbine power plant exhausting into a Deltak waste heat boiler to produce ''free'' process steam from the gas turbine exhaust, is discussed. The design includes water injection for NO/sub x/ control, self-cleaning inlet air filters, evaporative coolers, supercharger, and supplementary firing of the waste heat boiler. Once the system is operational Borax will be able to generate all of the electricity needed for on-site operations and a large share of process steam needs--plus still have 22-23 Mw surplus electric power to sell, so that the installation should pay for itself in lessmore » than 5 years of service.« less

N =4 supersymmetric mechanics on curved spaces

NASA Astrophysics Data System (ADS)

Kozyrev, Nikolay; Krivonos, Sergey; Lechtenfeld, Olaf; Nersessian, Armen; Sutulin, Anton

2018-04-01

We present N =4 supersymmetric mechanics on n -dimensional Riemannian manifolds constructed within the Hamiltonian approach. The structure functions entering the supercharges and the Hamiltonian obey modified covariant constancy equations as well as modified Witten-Dijkgraaf-Verlinde-Verlinde equations specified by the presence of the manifold's curvature tensor. Solutions of original Witten-Dijkgraaf-Verlinde-Verlinde equations and related prepotentials defining N =4 superconformal mechanics in flat space can be lifted to s o (n )-invariant Riemannian manifolds. For the Hamiltonian this lift generates an additional potential term which, on spheres and (two-sheeted) hyperboloids, becomes a Higgs-oscillator potential. In particular, the sum of n copies of one-dimensional conformal mechanics results in a specific superintegrable deformation of the Higgs oscillator.

S-Duality, Deconstruction and Confinement for a Marginal Deformation of N=4 SUSY Yang-Mills

NASA Astrophysics Data System (ADS)

Dorey, Nick

2004-08-01

We study an exactly marginal deformation of Script N = 4 SUSY Yang-Mills with gauge group U(N) using field theory and string theory methods. The classical theory has a Higgs branch for rational values of the deformation parameter. We argue that the quantum theory also has an S-dual confining branch which cannot be seen classically. The low-energy effective theory on these branches is a six-dimensional non-commutative gauge theory with sixteen supercharges. Confinement of magnetic and electric charges, on the Higgs and confining branches respectively, occurs due to the formation of BPS-saturated strings in the low energy theory. The results also suggest a new way of deconstructing Little String Theory as a large-N limit of a confining gauge theory in four dimensions.

Baseline performance and emissions data for a single-cylinder, direct-injected diesel engine

NASA Technical Reports Server (NTRS)

Dezelick, R. A.; Mcfadden, J. J.; Ream, L. W.; Barrows, R. F.

1983-01-01

Comprehensive fuel consumption, mean effective cylinder pressure, and emission test results for a supercharged, single-cylinder, direct-injected, four-stroke-cycle, diesel test engine are documented. Inlet air-to-exhaust pressure ratios were varied from 1.25 to 3.35 in order to establish the potential effects of turbocharging techniques on engine performance. Inlet air temperatures and pressures were adjusted from 34 to 107 C and from 193 to 414 kPa to determine the effects on engine performance and emissions. Engine output ranged from 300 to 2100 kPa (brake mean effective pressure) in the speed range of 1000 to 3000 rpm. Gaseous and particulate emission rates were measured. Real-time values of engine friction and pumping loop losses were measured independently and compared with motored engine values.

An Investigation of the Icing and Heated-air De-icing Characteristics of the R-2600-13 Induction System

NASA Technical Reports Server (NTRS)

Chapman, Gilbert E.

1946-01-01

A laboratory investigation was made on a Holley 1685-HB carburetor mounted on an R-2600-13 supercharger assembly to determine the icing characteristics and the heated-air de-icing requirements of this portion of the B-25D airplane induction system. Icing has been found to be most prevalent at relatively small throttle openings and, consequently, all runs were made at simulated 60-percent normal rated power condition. Icing characteristics were determined during a series of 15-minute runs over a range of inlet-air conditions. For the de-icing investigation severe impact ice was allowed to form in the induction system and the time required for the recovery of 95 percent of the maximum possible air flow at the original throttle setting was then determined for a range of wet-bulb temperatures. Results of these runs showed that ice on the walls of the carburetor adapter and on the rim of the impeller-shroud portion of the supercharger diffuser plate did not affect engine operation at 60-percent normal rated power. Ice that adversely affected the air flow and the fuel-air ratio was formed only on the central web of the carburetor and then only when the inlet air was saturated or contained free moisture in excess of saturation. No serious ice formations were observed at inlet-air temperatures above 66 0 F or with an inlet-air enthalpy greater than 34 Btu per pound. The maximum temperature at. which any trace of icing could be detected was 1110 F with a relative humidity of approximately 28 percent, The air-flow recovery time for emergency de-icing was 0.3 minute for.an enthalpy of 35 Btu per pound or wet-bulb temperature of 68 0 F. Further increase in enthalpy and wet-bulb temperature above these values resulted in very slight improvement in recovery time. The fuel-air ratio restored by a 5-Minute application of heated air was approximately 7 percent less than the initial value for cold-air conditions.

Minimum Specific Fuel Consumption of a Liquid-Cooled Multicylinder Aircraft Engine as Affected by Compression Ratio and Engine Operating Conditions

NASA Technical Reports Server (NTRS)

Brun, Rinaldo J.; Feder, Melvin S.; Harries, Myron L.

1947-01-01

An investigation was conducted on a 12-cylinder V-type liquid-cooled aircraft engine of 1710-cubic-inch displacement to determine the minimum specific fuel consumption at constant cruising engine speed and compression ratios of 6.65, 7.93, and 9.68. At each compression ratio, the effect.of the following variables was investigated at manifold pressures of 28, 34, 40, and 50 inches of mercury absolute: temperature of the inlet-air to the auxiliary-stage supercharger, fuel-air ratio, and spark advance. Standard sea-level atmospheric pressure was maintained at the auxiliary-stage supercharger inlet and the exhaust pressure was atmospheric. Advancing the spark timing from 34 deg and 28 deg B.T.C. (exhaust and intake, respectively) to 42 deg and 36 deg B.T.C. at a compression ratio of 6.65 resulted in a decrease of approximately 3 percent in brake specific fuel consumption. Further decreases in brake specific fuel consumption of 10.5 to 14.1 percent (depending on power level) were observed as the compression ratio was increased from 6.65 to 9.68, maintaining at each compression ratio the spark advance required for maximum torque at a fuel-air ratio of 0.06. This increase in compression ratio with a power output of 0.585 horsepower per cubic inch required a change from . a fuel- lend of 6-percent triptane with 94-percent 68--R fuel at a compression ratio of 6.65 to a fuel blend of 58-percent, triptane with 42-percent 28-R fuel at a compression ratio of 9.68 to provide for knock-free engine operation. As an aid in the evaluation of engine mechanical endurance, peak cylinder pressures were measured on a single-cylinder engine at several operating conditions. Peak cylinder pressures of 1900 pounds per square inch can be expected at a compression ratio of 9.68 and an indicated mean effective pressure of 320 pounds per square inch. The engine durability was considerably reduced at these conditions.

Euclidean supergravity

NASA Astrophysics Data System (ADS)

de Wit, Bernard; Reys, Valentin

2017-12-01

Supergravity with eight supercharges in a four-dimensional Euclidean space is constructed at the full non-linear level by performing an off-shell time-like reduction of five-dimensional supergravity. The resulting four-dimensional theory is realized off-shell with the Weyl, vector and tensor supermultiplets and a corresponding multiplet calculus. Hypermultiplets are included as well, but they are themselves only realized with on-shell supersymmetry. We also briefly discuss the non-linear supermultiplet. The off-shell reduction leads to a full understanding of the Euclidean theory. A complete multiplet calculus is presented along the lines of the Minkowskian theory. Unlike in Minkowski space, chiral and anti-chiral multiplets are real and supersymmetric actions are generally unbounded from below. Precisely as in the Minkowski case, where one has different formulations of Poincaré supergravity upon introducing different compensating supermultiplets, one can also obtain different versions of Euclidean supergravity.

Electric vehicle charging station quantity forecasting model

NASA Astrophysics Data System (ADS)

Dong, Yingshuai

2018-06-01

For both environmental and economic reasons, there is global interest in reducing the use of fossil fuels, including gasoline for cars. Whether motivated by the environment or by the economics, consumers are starting to migrate to electric vehicles. Tesla currently offers two types of charging stations: (1) destination charging designed for charging for several hours at a time or even overnight; and (2) supercharging designed for longer road trips to provide up to 170 miles of range in as little as 30 minutes of charging. These stations are in addition to at-home charging used by many Tesla owners who have a personal garage or a driveway with power. Based on private car survey data from the NHTS in the United States, this article predicts the number of charging stations required if everyone is using an electric passenger car across the United States.

Design study of an air pump and integral lift engine ALF-504 using the Lycoming 502 core

NASA Technical Reports Server (NTRS)

Rauch, D.

1972-01-01

Design studies were conducted for an integral lift fan engine utilizing the Lycoming 502 fan core with the final MQT power turbine. The fan is designed for a 12.5 bypass ratio and 1.25:1 pressure ratio, and provides supercharging for the core. Maximum sea level static thrust is 8370 pounds with a specific fuel consumption of 0.302 lb/hr-lb. The dry engine weight without starter is 1419 pounds including full-length duct and sound-attenuating rings. The engine envelope including duct treatment but not localized accessory protrusion is 53.25 inches in diameter and 59.2 inches long from exhaust nozzle exit to fan inlet flange. Detailed analyses include fan aerodynamics, fan and reduction gear mechanical design, fan dynamic analysis, engine noise analysis, engine performance, and weight analysis.

Solubilization of a membrane protein by combinatorial supercharging.

PubMed

Hajduczki, Agnes; Majumdar, Sudipta; Fricke, Marie; Brown, Isola A M; Weiss, Gregory A

2011-04-15

Hydrophobic and aggregation-prone, membrane proteins often prove too insoluble for conventional in vitro biochemical studies. To engineer soluble variants of human caveolin-1, a phage-displayed library of caveolin variants targeted the hydrophobic intramembrane domain with substitutions to charged residues. Anti-selections for insolubility removed hydrophobic variants, and positive selections for binding to the known caveolin ligand HIV gp41 isolated functional, folded variants. Assays with several caveolin binding partners demonstrated the successful folding and functionality by a solubilized, full-length caveolin variant selected from the library. This caveolin variant allowed assay of the direct interaction between caveolin and cavin. Clustered along one face of a putative helix, the solubilizing mutations suggest a structural model for the intramembrane domain of caveolin. The approach provides a potentially general method for solubilization and engineering of membrane-associated proteins by phage display.

The Origin and Diversification of Birds.

PubMed

Brusatte, Stephen L; O'Connor, Jingmai K; Jarvis, Erich D

2015-10-05

Birds are one of the most recognizable and diverse groups of modern vertebrates. Over the past two decades, a wealth of new fossil discoveries and phylogenetic and macroevolutionary studies has transformed our understanding of how birds originated and became so successful. Birds evolved from theropod dinosaurs during the Jurassic (around 165-150 million years ago) and their classic small, lightweight, feathered, and winged body plan was pieced together gradually over tens of millions of years of evolution rather than in one burst of innovation. Early birds diversified throughout the Jurassic and Cretaceous, becoming capable fliers with supercharged growth rates, but were decimated at the end-Cretaceous extinction alongside their close dinosaurian relatives. After the mass extinction, modern birds (members of the avian crown group) explosively diversified, culminating in more than 10,000 species distributed worldwide today. Copyright © 2015 Elsevier Ltd. All rights reserved.

Enzyme Encapsulation by a Ferritin Cage.

PubMed

Tetter, Stephan; Hilvert, Donald

2017-11-20

Ferritins, conserved across all kingdoms of life, are protein nanocages that evolved to mineralize iron. The last several decades have shown that these cages have considerable technological and medical potential owing to their stability and tolerance to modification, as well as their ability to template nanoparticle synthesis and incorporate small molecules. Here we show that it is possible to encapsulate proteins in a ferritin cage by exploiting electrostatic interactions with its negatively charged interior. Positively supercharged green fluorescent protein is efficiently taken up by Archaeoglobus fulgidus ferritin in a tunable fashion. Moreover, several enzymes were readily incorporated when genetically tethered to this fluorescent protein. These fusion proteins retained high catalytic activity and showed increased tolerance to proteolysis and heat. Equipping ferritins with enzymatic activity paves the way for many new nanotechnological and pharmacological applications. © 2017 Wiley-VCH Verlag GmbH & Co. KGaA, Weinheim.

What precision-protein-tuning and nano-resolved single molecule sciences can do for each other.

PubMed

Milles, Sigrid; Lemke, Edward A

2013-01-01

While innovations in modern microscopy, spectroscopy, and nanoscopy techniques have made single molecule observation a standard in many laboratories, the actual design of meaningful fluorescence reporter systems now hinders major scientific breakthroughs. Even though the field of chemical biology is supercharging the fluorescence toolbox, surprisingly few strategies exist that make the transition from model systems to biologically relevant applications. At the same time, the number of microscopy techniques is growing dramatically. We explain our view on how the impact of modern technologies is influenced not only by further hard- and software developments, but also by the availability and suitability of protein-engineering tools. We identify how the largely independent research fields of chemical biology and fluorescence nanoscopy can influence each other to synergistically drive future technology that can visualize the localization, structure, and dynamics of molecular function without constraints. Copyright © 2013 WILEY Periodicals, Inc.

Effects of Induction-System Icing on Aircraft-Engine Operating Characteristics

NASA Technical Reports Server (NTRS)

Stevens, Howard C., Jr.

1947-01-01

An investigation was conducted on a multicylinder aircraft engine on a dynamometer stand to determine the effect of induction-system icing on engine operating characteristics and to compare the results with those of a previous laboratory investigation in which only the carburetor and the engine-stage supercharger assembly from the engine were used. The experiments were conducted at simulated glide power, low cruise power, and normal rated power through a range of humidity ratios and air temperatures at approximately sea-level pressure. Induction-system icing was found to occur within approximately the same limits as those established by the previous laboratory investigation after making suitable allowances for the difference in fuel volatility and throttle angles. Rough operation of the engine was experienced when ice caused a marked reduction in the air flow. Photographs of typical ice formations from this investigation indicate close similarity to icing previously observed in the laboratory.

Compressor-fan unitary structure for air conditioning system

NASA Astrophysics Data System (ADS)

Dreiman, N.

2015-08-01

An extremely compact, therefore space saving unitary structure of short axial length is produced by radial integration of a revolving piston rotary compressor and an impeller of a centrifugal fan. The unitary structure employs single motor to run as the compressor so the airflow fan and eliminates duality of motors, related power supply and control elements. Novel revolving piston rotary compressor which provides possibility for such integration comprises the following: a suction gas delivery system which provides cooling of the motor and supplies refrigerant into the suction chamber under higher pressure (supercharged); a modified discharge system and lubricating oil supply system. Axial passages formed in the stationary crankshaft are used to supply discharge gas to a condenser, to return vaporized cooling agent from the evaporator to the suction cavity of the compressor, to pass a lubricant and to accommodate wiring supplying power to the unitary structure driver -external rotor electric motor.

GENENG 2: A program for calculating design and off-design performance of two- and three-spool turbofans with as many as three nozzles

NASA Technical Reports Server (NTRS)

Fishbach, L. H.; Koenig, R. W.

1972-01-01

A computer program which calculates steady-state design and off-design jet engine performance for two- or three-spool turbofans with one, two, or three nozzles is described. Included in the report are complete FORTRAN 4 listings of the program with sample results for nine basic turbofan engines that can be calculated: (1) three-spool, three-stream engine; (2) two-spool, three-stream, boosted-fan engine; (3) two-spool, three-stream, supercharged-compressor engine; (4) three-spool, two-stream engine; (5) two-spool, two-stream engine; (6) three-spool, three-stream, aft-fan engine; (7) two-spool, three-stream, aft-fan engine; (8) two-spool, two-stream, aft-engine; and (9) three-spool, two-stream, aft-fan engine. The simulation of other engines by using logical variables built into the program is also described.

Energy efficient engine: Fan test hardware detailed design report

NASA Technical Reports Server (NTRS)

Sullivan, T. J.

1980-01-01

A single stage fan and quarter stage booster were designed for the energy efficient engine. The fan has an inlet radius ratio of 0.342 and a specific flow rate of 208.9 Kg/S sq m (42.8 lbm/sec sq ft). The fan rotor has 32 medium aspect ratio (2.597) titanium blades with a partspan shroud at 55% blade height. The design corrected fan tip speed is 411.5 M/S (1350 ft/sec). The quarter stage island splits the total fan flow with approximately 22% of the flow being supercharged by the quarter stage rotor. The fan bypass ratio is 6.8. The core flow total pressure ratio is 1.67 and the fan bypass pressure ratio is 1.65. The design details of the fan and booster blading, and the fan frame and static structure for the fan configuration are presented.

Research and Improvement on Characteristics of Emergency Diesel Generating Set Mechanical Support System in Nuclear Power Plant

NASA Astrophysics Data System (ADS)

Zhe, Yang

2017-06-01

There are often mechanical problems of emergency power generation units in nuclear power plant, which bring a great threat to nuclear safety. Through analyzing the influence factors caused by mechanical failure, the existing defects of the design of mechanical support system are determined, and the design idea has caused the direction misleading in the field of maintenance and transformation. In this paper, research analysis is made on basic support design of diesel generator set, main pipe support design and important components of supercharger support design. And this paper points out the specific design flaws and shortcomings, and proposes targeted improvement program. Through the implementation of improvement programs, vibration level of unit and mechanical failure rate are reduced effectively. At the same time, it also provides guidance for design, maintenance and renovation of diesel generator mechanical support system of nuclear power plants in the future.

DOE Office of Scientific and Technical Information (OSTI.GOV)

Marquette, Ian, E-mail: i.marquette@uq.edu.au; Quesne, Christiane, E-mail: cquesne@ulb.ac.be

The purpose of this communication is to point out the connection between a 1D quantum Hamiltonian involving the fourth Painlevé transcendent P{sub IV}, obtained in the context of second-order supersymmetric quantum mechanics and third-order ladder operators, with a hierarchy of families of quantum systems called k-step rational extensions of the harmonic oscillator and related with multi-indexed X{sub m{sub 1,m{sub 2,…,m{sub k}}}} Hermite exceptional orthogonal polynomials of type III. The connection between these exactly solvable models is established at the level of the equivalence of the Hamiltonians using rational solutions of the fourth Painlevé equation in terms of generalized Hermite andmore » Okamoto polynomials. We also relate the different ladder operators obtained by various combinations of supersymmetric constructions involving Darboux-Crum and Krein-Adler supercharges, their zero modes and the corresponding energies. These results will demonstrate and clarify the relation observed for a particular case in previous papers.« less

The Effect of Piston-Head Temperature on Knock-Limited Power

NASA Technical Reports Server (NTRS)

Imming, Harry S.

1944-01-01

To determine the effect of piston-head temperature on knock-limited power. Tests were made in a supercharged CFR engine over a range of fuel-air ratios from 0.055 to 0.120, using S-3 reference fuel, AN-F-28, Amendment-2, aviation gasoline, and AN-F-28 plus 2 percent xylidines by weight. Tests were run at a compression ratio of 7.0 with inlet-air temperatures of 150 F and 250 F and at a compression ratio of 8.0 with an inlet-air temperature of 250 F. All other engine conditions were held constant. The piston-head temperature was varied by circulation of oil through passages in the crown of a liquid-cooled piston. This method of piston cooling decreased the piston-head temperature about 80 F. The data are not intended to constitute a recommendation as to the advisability of piston cooling in practice.

Assessment of the effect of gaseous fuel delivery mode on thermal efficiency and fuel losses during the valve overlap period in a dual-fuel compression ignition engine

NASA Astrophysics Data System (ADS)

Skrzek, T.

2016-09-01

The paper describes the effect of dual fuelling of single cylinder AVL test CI engine with the use of two ways of gas delivery to the engine manifold. The engine was fuelled diesel oil and propane. For all the tests, gas consumption was maintained at the same level. In the first mode the gas was delivered by injector located under inlet valve. In the second method, there was used a mixer fitted to the intake manifold. The paper compares the results of thermal efficiency and emissions of propane in the exhaust for both fuelling modes. Research clearly show how important it is to synchronize the injector opening time of the intake stroke. This is especially important for supercharged engines in which there is a valve overlap.

A method of calculating the performance of controllable propellers with sample computations

NASA Technical Reports Server (NTRS)

Hartman, Edwin P

1934-01-01

This paper contains a series of calculations showing how the performance of controllable propellers may be derived from data on fixed-pitch propellers given in N.A.C.A. Technical Report No. 350, or from similar data. Sample calculations are given which compare the performance of airplanes with fixed-pitch and with controllable propellers. The gain in performance with controllable propellers is shown to be largely due to the increased power available, rather than to an increase in efficiency. Controllable propellers are of particular advantage when used with geared and with supercharged engines. A controllable propeller reduces the take-off run, increases the rate of climb and the ceiling, but does not increase the high speed, except when operating above the design altitude of the previously used fixed-pitch propeller or when that propeller was designed for other than high speed.

Structure and assembly of scalable porous protein cages

NASA Astrophysics Data System (ADS)

Sasaki, Eita; Böhringer, Daniel; van de Waterbeemd, Michiel; Leibundgut, Marc; Zschoche, Reinhard; Heck, Albert J. R.; Ban, Nenad; Hilvert, Donald

2017-03-01

Proteins that self-assemble into regular shell-like polyhedra are useful, both in nature and in the laboratory, as molecular containers. Here we describe cryo-electron microscopy (EM) structures of two versatile encapsulation systems that exploit engineered electrostatic interactions for cargo loading. We show that increasing the number of negative charges on the lumenal surface of lumazine synthase, a protein that naturally assembles into a ~1-MDa dodecahedron composed of 12 pentamers, induces stepwise expansion of the native protein shell, giving rise to thermostable ~3-MDa and ~6-MDa assemblies containing 180 and 360 subunits, respectively. Remarkably, these expanded particles assume unprecedented tetrahedrally and icosahedrally symmetric structures constructed entirely from pentameric units. Large keyhole-shaped pores in the shell, not present in the wild-type capsid, enable diffusion-limited encapsulation of complementarily charged guests. The structures of these supercharged assemblies demonstrate how programmed electrostatic effects can be effectively harnessed to tailor the architecture and properties of protein cages.

V/STOL model fan stage rig design report

NASA Technical Reports Server (NTRS)

Cheatham, J. G.; Creason, T. L.

1983-01-01

A model single-stage fan with variable inlet guide vanes (VIGV) was designed to demonstrate efficient point operation while providing flow and pressure ratio modulation capability required for a V/STOL propulsion system. The fan stage incorporates a split-flap VIGV with an independently actuated ID flap to permit independent modulation of fan and core engine airstreams, a flow splitter integrally designed into the blade and vanes to completely segregate fan and core airstreams in order to maximize core stream supercharging for V/STOL operation, and an EGV with a variable leading edge fan flap for rig performance optimization. The stage was designed for a maximum flow size of 37.4 kg/s (82.3 lb/s) for compatibility with LeRC test facility requirements. Design values at maximum flow for blade tip velocity and stage pressure ratio are 472 m/s (1550 ft/s) and 1.68, respectively.

Spin(7) compactifications and 1/4-BPS vacua in heterotic supergravity

NASA Astrophysics Data System (ADS)

Angus, Stephen; Matti, Cyril; Svanes, Eirik E.

2016-03-01

We continue the investigation into non-maximally symmetric compactifications of the heterotic string. In particular, we consider compactifications where the internal space is allowed to depend on two or more external directions. For preservation of supersymmetry, this implies that the internal space must in general be that of a Spin(7) manifold, which leads to a 1/4-BPS four-dimensional supersymmetric perturbative vacuum breaking all but one supercharge. We find that these solutions allow for internal geometries previously excluded by the domain-wall-type solutions, and hence the resulting four-dimensional superpotential is more generic. In particular, we find an interesting resemblance to the superpotentials that appear in non-geometric flux compactifications of type II string theory. If the vacua are to be used for phenomenological applications, they must be lifted to maximal symmetry by some non-perturbative or higher-order effect.

Testing the effectiveness and the contribution of experimental supercharge (reversed) end-to-side nerve transfer.

PubMed

Nadi, Mustafa; Ramachandran, Sudheesh; Islam, Abir; Forden, Joanne; Guo, Gui Fang; Midha, Rajiv

2018-05-18

OBJECTIVE Supercharge end-to-side (SETS) transfer, also referred to as reverse end-to-side transfer, distal to severe nerve compression neuropathy or in-continuity nerve injury is gaining clinical popularity despite questions about its effectiveness. Here, the authors examined SETS distal to experimental neuroma in-continuity (NIC) injuries for efficacy in enhancing neuronal regeneration and functional outcome, and, for the first time, they definitively evaluated the degree of contribution of the native and donor motor neuron pools. METHODS This study was conducted in 2 phases. In phase I, rats (n = 35) were assigned to one of 5 groups for unilateral sciatic nerve surgeries: group 1, tibial NIC with distal peroneal-tibial SETS; group 2, tibial NIC without SETS; group 3, intact tibial and severed peroneal nerves; group 4, tibial transection with SETS; and group 5, severed tibial and peroneal nerves. Recovery was evaluated biweekly using electrophysiology and locomotion tasks. At the phase I end point, after retrograde labeling, the spinal cords were analyzed to assess the degree of neuronal regeneration. In phase II, 20 new animals underwent primary retrograde labeling of the tibial nerve, following which they were assigned to one of the following 3 groups: group 1, group 2, and group 4. Then, secondary retrograde labeling from the tibial nerve was performed at the study end point to quantify the native versus donor regenerated neuronal pool. RESULTS In phase I studies, a significantly increased neuronal regeneration in group 1 (SETS) compared with all other groups was observed, but with modest (nonsignificant) improvement in electrophysiological and behavioral outcomes. In phase II experiments, the authors discovered that secondary labeling in group 1 was predominantly contributed from the donor (peroneal) pool. Double-labeling counts were dramatically higher in group 2 than in group 1, suggestive of hampered regeneration from the native tibial motor neuron pool across the NIC segment in the presence of SETS. CONCLUSIONS SETS is indeed an effective strategy to enhance axonal regeneration, which is mainly contributed by the donor neuronal pool. Moreover, the presence of a distal SETS coaptation appears to negatively influence neuronal regeneration across the NIC segment. The clinical significance is that SETS should only employ synergistic donors, as the use of antagonistic donors can downgrade recovery.

Remaining Technical Challenges and Future Plans for Oil-Free Turbomachinery

NASA Technical Reports Server (NTRS)

DellaCorte, Christopher; Bruckner, Robert J.

2010-01-01

The application of Oil-Free technologies (foil gas bearings, solid lubricants and advanced analysis and predictive modeling tools) to advanced turbomachinery has been underway for several decades. During that time, full commercialization has occurred in aircraft air cycle machines, turbocompressors and cryocoolers and ever-larger microturbines. Emerging products in the automotive sector (turbochargers and superchargers) indicate that high volume serial production of foil bearings is imminent. Demonstration of foil bearings in APU s and select locations in propulsion gas turbines illustrates that such technology also has a place in these future systems. Foil bearing designs, predictive tools and advanced solid lubricants have been reported that can satisfy anticipated requirements but a major question remains regarding the scalability of foil bearings to ever larger sizes to support heavier rotors. In this paper, the technological history, primary physics, engineering practicalities and existing experimental and experiential database for scaling foil bearings are reviewed and the major remaining technical challenges are identified.

Fuels and Lubrication Researcher at the Aircraft Engine Research Laboratory

NASA Image and Video Library

1943-08-21

A researcher at the National Advisory Committee for Aeronautics (NACA) Aircraft Engine Research Laboratory studies the fuel ignition process. Improved fuels and lubrication was an area of particular emphasis at the laboratory during World War II. The military sought to use existing types of piston engines in order to get large numbers of aircraft into the air as quickly as possible. To accomplish its goals, however, the military needed to increase the performance of these engines without having to wait for new models or extensive redesigns. The Aircraft Engine Research Laboratory was called on to lead this effort. The use of superchargers successfully enhanced engine performance, but the resulting heat increased engine knock [fuel detonation] and structural wear. These effects could be offset with improved cooling, lubrication, and fuel mixtures. The NACA researchers in the Fuels and Lubrication Division concentrated on new synthetic fuels, higher octane fuels, and fuel-injection systems. The laboratory studied 16 different types of fuel blends during the war, including extensive investigations of triptane and xylidine.

Anomaly-corrected supersymmetry algebra and supersymmetric holographic renormalization

NASA Astrophysics Data System (ADS)

An, Ok Song

2017-12-01

We present a systematic approach to supersymmetric holographic renormalization for a generic 5D N=2 gauged supergravity theory with matter multiplets, including its fermionic sector, with all gauge fields consistently set to zero. We determine the complete set of supersymmetric local boundary counterterms, including the finite counterterms that parameterize the choice of supersymmetric renormalization scheme. This allows us to derive holographically the superconformal Ward identities of a 4D superconformal field theory on a generic background, including the Weyl and super-Weyl anomalies. Moreover, we show that these anomalies satisfy the Wess-Zumino consistency condition. The super-Weyl anomaly implies that the fermionic operators of the dual field theory, such as the supercurrent, do not transform as tensors under rigid supersymmetry on backgrounds that admit a conformal Killing spinor, and their anticommutator with the conserved supercharge contains anomalous terms. This property is explicitly checked for a toy model. Finally, using the anomalous transformation of the supercurrent, we obtain the anomaly-corrected supersymmetry algebra on curved backgrounds admitting a conformal Killing spinor.

Modeling the internal combustion engine

NASA Technical Reports Server (NTRS)

Zeleznik, F. J.; Mcbride, B. J.

1985-01-01

A flexible and computationally economical model of the internal combustion engine was developed for use on large digital computer systems. It is based on a system of ordinary differential equations for cylinder-averaged properties. The computer program is capable of multicycle calculations, with some parameters varying from cycle to cycle, and has restart capabilities. It can accommodate a broad spectrum of reactants, permits changes in physical properties, and offers a wide selection of alternative modeling functions without any reprogramming. It readily adapts to the amount of information available in a particular case because the model is in fact a hierarchy of five models. The models range from a simple model requiring only thermodynamic properties to a complex model demanding full combustion kinetics, transport properties, and poppet valve flow characteristics. Among its many features the model includes heat transfer, valve timing, supercharging, motoring, finite burning rates, cycle-to-cycle variations in air-fuel ratio, humid air, residual and recirculated exhaust gas, and full combustion kinetics.

Numerical Investigation of Flow in a Centrifugal Compressor

NASA Astrophysics Data System (ADS)

Grishin, Yu. A.; Bakulin, V. N.

2015-09-01

With the use of the domestic software suite of computational hydrodynamics Flow Vision based on application of the method of control volumes, numerical simulation of air composition and delivery by a centrifugal compressor employed for supercharging a piston engine has been carried out. The head-flow characteristics of the compressor, as well as the 3D fields of flow velocity and pressure distributions in the elements of the compressor flow passage, including the interblade channels of the impeller, have been obtained for various regimes. In the regimes of diminished air flow rate, surging phenomena are identified, characterized by a return flow. The application of the technique of numerical experiment will make it possible from here on to carry out design optimization of the compressor flow passage profile and thus to improve its basic characteristics — the degree of pressure increase, compressed air flow rate, and the efficiency — as well as to reduce the costs of the development and production of compressors.

Schwarzschild radius from Monte Carlo calculation of the Wilson loop in supersymmetric matrix quantum mechanics.

PubMed

Hanada, Masanori; Miwa, Akitsugu; Nishimura, Jun; Takeuchi, Shingo

2009-05-08

In the string-gauge duality it is important to understand how the space-time geometry is encoded in gauge theory observables. We address this issue in the case of the D0-brane system at finite temperature T. Based on the duality, the temporal Wilson loop W in gauge theory is expected to contain the information of the Schwarzschild radius RSch of the dual black hole geometry as log(W)=RSch/(2pialpha'T). This translates to the power-law behavior log(W)=1.89(T/lambda 1/3)-3/5, where lambda is the 't Hooft coupling constant. We calculate the Wilson loop on the gauge theory side in the strongly coupled regime by performing Monte Carlo simulations of supersymmetric matrix quantum mechanics with 16 supercharges. The results reproduce the expected power-law behavior up to a constant shift, which is explainable as alpha' corrections on the gravity side. Our conclusion also demonstrates manifestly the fuzzball picture of black holes.

Connection between quantum systems involving the fourth Painlevé transcendent and k-step rational extensions of the harmonic oscillator related to Hermite exceptional orthogonal polynomial

NASA Astrophysics Data System (ADS)

Marquette, Ian; Quesne, Christiane

2016-05-01

The purpose of this communication is to point out the connection between a 1D quantum Hamiltonian involving the fourth Painlevé transcendent PIV, obtained in the context of second-order supersymmetric quantum mechanics and third-order ladder operators, with a hierarchy of families of quantum systems called k-step rational extensions of the harmonic oscillator and related with multi-indexed Xm1,m2,…,mk Hermite exceptional orthogonal polynomials of type III. The connection between these exactly solvable models is established at the level of the equivalence of the Hamiltonians using rational solutions of the fourth Painlevé equation in terms of generalized Hermite and Okamoto polynomials. We also relate the different ladder operators obtained by various combinations of supersymmetric constructions involving Darboux-Crum and Krein-Adler supercharges, their zero modes and the corresponding energies. These results will demonstrate and clarify the relation observed for a particular case in previous papers.

M5-brane and D-brane scattering amplitudes

NASA Astrophysics Data System (ADS)

Heydeman, Matthew; Schwarz, John H.; Wen, Congkao

2017-12-01

We present tree-level n-particle on-shell scattering amplitudes of various brane theories with 16 conserved supercharges. These include the world-volume theory of a probe D3-brane or D5-brane in 10D Minkowski spacetime as well as a probe M5-brane in 11D Minkowski spacetime, which describes self interactions of an abelian tensor supermultiplet with 6D (2, 0) supersymmetry. Twistor-string-like formulas are proposed for tree-level scattering amplitudes of all multiplicities for each of these theories. The R symmetry of the D3-brane theory is shown to be SU(4) × U(1), and the U(1) factor implies that its amplitudes are helicity conserving. Each of 6D theories (D5-brane and M5-brane) reduces to the D3-brane theory by dimensional reduction. As special cases of the general M5-brane amplitudes, we present compact formulas for examples involving only the self-dual B field with n = 4, 6, 8.

Propfan test assessment propfan propulsion system static test report

NASA Technical Reports Server (NTRS)

Orourke, D. M.

1987-01-01

The propfan test assessment (PTA) propulsion system successfully completed over 50 hours of extensive static ground tests, including a 36 hour endurance test. All major systems performed as expected, verifying that the large-scale 2.74 m diameter propfan, engine, gearbox, controls, subsystems, and flight instrumentation will be satisfactory with minor modifications for the upcoming PTA flight tests on the GII aircraft in early 1987. A test envelope was established for static ground operation to maintain propfan blade stresses within limits for propfan rotational speeds up to 105 percent and power levels up to 3880 kW. Transient tests verified stable, predictable response of engine power and propfan speed controls. Installed engine TSFC was better than expected, probably due to the excellent inlet performance coupled with the supercharging effect of the propfan. Near- and far-field noise spectra contained three dominant components, which were dependent on power, tip speed, and direction. The components were propfan blade tones, propfan random noise, and compressor/propfan interaction noise. No significant turbine noise or combustion noise was evident.

DOE Office of Scientific and Technical Information (OSTI.GOV)

Essman, Eric P.; Aganagic, Mina; Okuda, Takuya

We study quantum entanglements of baby universes which appear in non-perturbative corrections to the OSV formula for the entropy of extremal black holes in type IIA string theory compactified on the local Calabi-Yau manifold defined as a rank 2 vector bundle over an arbitrary genus G Riemann surface. This generalizes the result for G=1 in hep-th/0504221. Non-perturbative terms can be organized into a sum over contributions from baby universes, and the total wave-function is their coherent superposition in the third quantized Hilbert space. We find that half of the universes preserve one set of supercharges while the other half preservemore » a different set, making the total universe stable but non-BPS. The parent universe generates baby universes by brane/anti-brane pair creation, and baby universes are correlated by conservation of non-normalizable D-brane charges under the process. There are no other source of entanglement of baby universes, and all possible states are superposed with the equal weight.« less

Intersecting surface defects and two-dimensional CFT

NASA Astrophysics Data System (ADS)

Gomis, Jaume; Le Floch, Bruno; Pan, Yiwen; Peelaers, Wolfger

2017-08-01

We initiate the study of intersecting surface operators/defects in 4D quantum field theories (QFTs). We characterize these defects by coupled 4D/2D/0D theories constructed by coupling the degrees of freedom localized at a point and on intersecting surfaces in spacetime to each other and to the 4D QFT. We construct supersymmetric intersecting surface defects preserving just two supercharges in N =2 gauge theories. These defects are amenable to exact analysis by localization of the partition function of the underlying 4D/2D/0D QFT. We identify the 4D/2D/0D QFTs that describe intersecting surface operators in N =2 gauge theories realized by intersecting M2 branes ending on N M5 branes wrapping a Riemann surface. We conjecture and provide evidence for an explicit equivalence between the squashed four-sphere partition function of these intersecting defects and correlation functions in Liouville/Toda CFT with the insertion of arbitrary degenerate vertex operators, which are labeled by two representations of S U (N ).

Topological quantum computation of the Dold-Thom functor

NASA Astrophysics Data System (ADS)

Ospina, Juan

2014-05-01

A possible topological quantum computation of the Dold-Thom functor is presented. The method that will be used is the following: a) Certain 1+1-topological quantum field theories valued in symmetric bimonoidal categories are converted into stable homotopical data, using a machinery recently introduced by Elmendorf and Mandell; b) we exploit, in this framework, two recent results (independent of each other) on refinements of Khovanov homology: our refinement into a module over the connective k-theory spectrum and a stronger result by Lipshitz and Sarkar refining Khovanov homology into a stable homotopy type; c) starting from the Khovanov homotopy the Dold-Thom functor is constructed; d) the full construction is formulated as a topological quantum algorithm. It is conjectured that the Jones polynomial can be described as the analytical index of certain Dirac operator defined in the context of the Khovanov homotopy using the Dold-Thom functor. As a line for future research is interesting to study the corresponding supersymmetric model for which the Khovanov-Dirac operator plays the role of a supercharge.

Hybrid and conventional hydrogen engine vehicles that meet EZEV emissions

DOE Office of Scientific and Technical Information (OSTI.GOV)

Aceves, S.M.; Smith, J.R.

In this paper, a time-dependent engine model is used for predicting hydrogen engine efficiency and emissions. The model uses basic thermodynamic equations for the compression and expansion processes, along with an empirical correlation for heat transfer, to predict engine indicated efficiency. A friction correlation and a supercharger/turbocharger model are then used to calculate brake thermal efficiency. The model is validated with many experimental points obtained in a recent evaluation of a hydrogen research engine. A The validated engine model is then used to calculate fuel economy and emissions for three hydrogen-fueled vehicles: a conventional, a parallel hybrid, and a seriesmore » hybrid. All vehicles use liquid hydrogen as a fuel. The hybrid vehicles use a flywheel for energy storage. Comparable ultra capacitor or battery energy storage performance would give similar results. This paper analyzes the engine and flywheel sizing requirements for obtaining a desired level of performance. The results indicate that hydrogen lean-burn spark-ignited engines can provide a high fuel economy and Equivalent Zero Emission Vehicle (EZEV) levels in the three vehicle configurations being analyzed.« less

A locally supersymmetric SO(10, 2) invariant action for D = 12 supergravity

NASA Astrophysics Data System (ADS)

Castellani, Leonardo

2017-06-01

We present an action for N = 1 supergravity in 10 + 2 dimensions, containing the gauge fields of the OSp(1|64) superalgebra, i.e. one-forms B ( n) with n=1,2,5,6,9,10 antisymmetric D=12 Lorentz indices and a Majorana gravitino ψ. The vielbein and spin connection correspond to B (1) and B (2) respectively. The action is not gauge invariant under the full OSp(1|64) superalgebra, but only under a subalgebra \\tilde{F} (containing the F algebra OSp(1|32)), whose gauge fields are B (2), B (6), B (10) and the Weyl projected Majorana gravitino 1/2(1+{Γ}_{13})ψ . Supersymmetry transformations are therefore generated by a Majorana-Weyl supercharge and, being part of a gauge superalgebra, close off-shell. The action is simply ∫ STr( R 6 Γ) where R is the OSp(1|64) curvature supermatrix two-form, and Γ is a constant supermatrix involving Γ13 and breaking OSp(1|64) to its \\tilde{F} subalgebra. The usual Einstein-Hilbert term is included in the action.

Triality in little string theories

NASA Astrophysics Data System (ADS)

Bastian, Brice; Hohenegger, Stefan; Iqbal, Amer; Rey, Soo-Jong

2018-02-01

We study a class of eight-supercharge little string theories (LSTs) on the world volume of N M5-branes with transverse space S1×(C2/ZM). These M-brane configurations compactified on a circle are dual to M D5-branes intersecting N NS5-branes on T2×R7 ,1 as well as to F-theory compactified on a toric Calabi-Yau threefold XN ,M. We argue that the Kähler cone of XN ,M admits three regions associated with weakly coupled quiver gauge theories of gauge groups [U (N )]M,[U (M )]N, and [U (N/M k )]k where k =gcd (N ,M ). These provide low-energy descriptions of different LSTs. The duality between the first two gauge theories is well known and is a consequence of the S-duality between D5- and NS5-branes or the T-duality of the LSTs. The triality involving the third gauge theory is new, and we demonstrate it using several examples. We also discuss implications of this triality for the W-algebras associated with the Alday-Gaiotto-Tachikawa dual theories.

Integrands for QCD rational terms and {N} = {4} SYM from massive CSW rules

NASA Astrophysics Data System (ADS)

Elvang, Henriette; Freedman, Daniel Z.; Kiermaier, Michael

2012-06-01

We use massive CSW rules to derive explicit compact expressions for integrands of rational terms in QCD with any number of external legs. Specifically, we present all- n integrands for the one-loop all-plus and one-minus gluon amplitudes in QCD. We extract the finite part of spurious external-bubble contributions systematically; this is crucial for the application of integrand-level CSW rules in theories without supersymmetry. Our approach yields integrands that are independent of the choice of CSW reference spinor even before integration. Furthermore, we present a recursive derivation of the recently proposed massive CSW-style vertex expansion for massive tree amplitudes and loop integrands on the Coulomb-branch of {N} = {4} SYM. The derivation requires a careful study of boundary terms in all-line shift recursion relations, and provides a rigorous (albeit indirect) proof of the recently proposed construction of massive amplitudes from soft-limits of massless on-shell amplitudes. We show that the massive vertex expansion manifestly preserves all holomorphic and half of the anti-holomorphic supercharges, diagram-by-diagram, even off-shell.

Quantum integrable systems from conformal blocks

NASA Astrophysics Data System (ADS)

Chen, Heng-Yu; Qualls, Joshua D.

2017-05-01

In this note, we extend the striking connections between quantum integrable systems and conformal blocks recently found in [M. Isachenkov and V. Schomerus, Phys. Rev. Lett. 117, 071602 (2016), 10.1103/PhysRevLett.117.071602] in several directions. First, we explicitly demonstrate that the action of the quartic conformal Casimir operator on general d-dimensional scalar conformal blocks can be expressed in terms of certain combinations of commuting integrals of motions of the two particle hyperbolic BC2 Calogero-Sutherland system. The permutation and reflection properties of the underlying Dunkl operators play crucial roles in establishing such a connection. Next, we show that the scalar superconformal blocks in superconformal field theories (SCFTs) with four and eight supercharges and suitable chirality constraints can also be identified with the eigenfunctions of the same Calogero-Sutherland system; this demonstrates the universality of such a connection. Finally, we observe that the so-called "seed" conformal blocks for constructing four point functions for operators with arbitrary space-time spins in four-dimensional CFTs can also be linearly expanded in terms of Calogero-Sutherland eigenfunctions.

Icing-Protection Requirements for Reciprocating-Engine Induction System

NASA Technical Reports Server (NTRS)

Coles, Willard D; Rollin, Vern G; Mulholland, Donald R

1950-01-01

Despite the development of relatively ice-free fuel-metering systems, the widespread use of alternate and heated-air intakes, and the use of alcohol for emergency de-icing, icing of aircraft-engine induction systems is a serious problem. Investigations have been made to study and to combat all phases of this icing problem. From these investigations, criterions for safe operation and for design of new induction systems have been established. The results were obtained from laboratory investigations of carburetor-supercharger combinations, wind-tunnel investigations of air scoops, multicylinder-engine studies, and flight investigations. Characteristics of three forms of ice, impact, throttling, and fuel evaporation were studied. The effects of several factors on the icing characteristics were also studied and included: (1) atmospheric conditions, (2) engine and air-scoop configurations, including light-airplane system, (3) type fuel used, and (4) operating variables, such as power condition, use of a manifold pressure regulator, mixture setting, carburetor heat, and water-alcohol injection. In addition, ice-detection methods were investigated and methods of preventing and removing induction-system ice were studied. Recommendations are given for design and operation with regard to induction-system design.

Deformed oscillator algebra approach of some quantum superintegrable Lissajous systems on the sphere and of their rational extensions

DOE Office of Scientific and Technical Information (OSTI.GOV)

Marquette, Ian, E-mail: i.marquette@uq.edu.au; Quesne, Christiane, E-mail: cquesne@ulb.ac.be

2015-06-15

We extend the construction of 2D superintegrable Hamiltonians with separation of variables in spherical coordinates using combinations of shift, ladder, and supercharge operators to models involving rational extensions of the two-parameter Lissajous systems on the sphere. These new families of superintegrable systems with integrals of arbitrary order are connected with Jacobi exceptional orthogonal polynomials of type I (or II) and supersymmetric quantum mechanics. Moreover, we present an algebraic derivation of the degenerate energy spectrum for the one- and two-parameter Lissajous systems and the rationally extended models. These results are based on finitely generated polynomial algebras, Casimir operators, realizations as deformedmore » oscillator algebras, and finite-dimensional unitary representations. Such results have only been established so far for 2D superintegrable systems separable in Cartesian coordinates, which are related to a class of polynomial algebras that display a simpler structure. We also point out how the structure function of these deformed oscillator algebras is directly related with the generalized Heisenberg algebras spanned by the nonpolynomial integrals.« less

Rotary internal combustion engine with integrated supercharged fuel-air induction

DOE Office of Scientific and Technical Information (OSTI.GOV)

Southard, A.A.

This patent describes an improved method of operating a rotary internal combustion engine of the type wherein a multicusped rotor rotatable upon a rotatable eccentric rotates within a cavity bounded by a wall of lobed trochoidal configuration. The rotor cusps have sealing engagement separating and defining operating chambers in the cavity about the rotor between adjacent pairs of cusps. Such chambers are angularly spaced about and orbit the center of the cavity as the rotor rotates while each chamber alternately expands and contracts in volume. The method comprises cylindrically operating each chamber through a sequence of six phases that aremore » synchronized with three successive increases and decreases in the volume of such chamber, with the first four phases being an internal combustion engine power cycle comprising an air intake phase, a compression phase, a combustion phase and an exhaust phase. The fifth phase comprises inducting air into the chamber, and the sixth phase comprises compressing the inducted air in such chamber and passing such inducted and compressed air through an elongated transfer zone.« less

Effect of Several Factors on the Cooling of a Radial Engine in Flight

NASA Technical Reports Server (NTRS)

Schey, Oscar W; Pinkel, Benjamin

1936-01-01

Flight tests of a Grumman Scout (XSF-2) airplane fitted with a Pratt & Whitney 1535 supercharged engine were conducted to determine the effect of engine power, mass flow of the cooling air, and atmospheric temperature on cylinder temperature. The tests indicated that the difference in temperature between the cylinder wall and the cooling air varied as the 0.38 power of the brake horsepower for a constant mass flow of cooling air, cooling-air temperature, engine speed, and brake fuel consumption. The difference in temperature was also found to vary inversely as the 0.39 power of the mass flow for points on the head and the 0.35 power for points on the barrel, provided that engine power, engine speed, brake fuel consumption, and cooling-air temperature were kept constant. The results of the tests of the effect of atmospheric temperature on cylinder temperature were inconclusive owing to unfavorable weather conditions prevailing at the time of the tests. The method used for controlling the test conditions, however, was found to be feasible.

Fabrication Division Staff in the Machine Shop

NASA Image and Video Library

1946-07-21

Machine Shop technicians in the Technical Service Building at the National Advisory Committee for Aeronautics (NACA) Lewis Flight Propulsion Laboratory. The 260-person Fabrication Division, led by Dan White and John Dalgleish, created almost all of the equipment and models used at the laboratory. The Technical Services Building, referred to as the Fab Shop, contained a number of specialized shops in the 1940s and 1950s. These included a Machine Shop, Sheet Metal Shop, Wood and Pattern Shop, Instrument Shop, Thermocouple Shop, Heat Treating Shop, Metallurgical Laboratory, and Fabrication Office. The Machine Shop fabricated specialized research equipment not commercially available. During World War II these technicians produced high-speed cameras for combustion research, impellers and other supercharger components, and key equipment for the lab’s first supersonic wind tunnel. The Wood and Pattern Shop created everything from control panels and cabinets to aircraft model molds for sheet metal work. The Sheet Metal Shop had the ability to work with 0.01 to 4-inch thick steel plates. The Instrument Shop specialized in miniature parts and instrumentation, while the Thermocouple Shop standardized the installation of pitot tubes and thermocouples.

Gauge supergravity in D = 2 + 2

NASA Astrophysics Data System (ADS)

Castellani, Leonardo

2017-10-01

We present an action for chiral N = (1 , 0) supergravity in 2 + 2 dimensions. The fields of the theory are organized into an OSp(1|4) connection supermatrix, and are given by the usual vierbein V a , spin connection ω ab , and Majorana gravitino ψ. In analogy with a construction used for D = 10 + 2 gauge supergravity, the action is given by ∫STr( R 2 Γ), where R is the OSp(1|4) curvature supermatrix two-form, and Γ a constant supermatrix containing γ 5. It is similar, but not identical to the MacDowell-Mansouri action for D = 2 + 2 supergravity. The constant supermatrix breaks OSp(1|4) gauge invariance to a subalgebra OSp(1|2) ⊕ Sp(2), including a Majorana-Weyl supercharge. Thus half of the OSp(1|4) gauge supersymmetry survives. The gauge fields are the selfdual part of ω ab and the Weyl projection of ψ for OSp(1|2), and the antiselfdual part of ω ab for Sp(2). Supersymmetry transformations, being part of a gauge superalgebra, close off-shell. The selfduality condition on the spin connection can be consistently imposed, and the resulting "projected" action is OSp(1|2) gauge invariant.

Branes and the Kraft-Procesi transition: classical case

NASA Astrophysics Data System (ADS)

Cabrera, Santiago; Hanany, Amihay

2018-04-01

Moduli spaces of a large set of 3 d N=4 effective gauge theories are known to be closures of nilpotent orbits. This set of theories has recently acquired a special status, due to Namikawa's theorem. As a consequence of this theorem, closures of nilpotent orbits are the simplest non-trivial moduli spaces that can be found in three dimensional theories with eight supercharges. In the early 80's mathematicians Hanspeter Kraft and Claudio Procesi characterized an inclusion relation between nilpotent orbit closures of the same classical Lie algebra. We recently [1] showed a physical realization of their work in terms of the motion of D3-branes on the Type IIB superstring embedding of the effective gauge theories. This analysis is restricted to A-type Lie algebras. The present note expands our previous discussion to the remaining classical cases: orthogonal and symplectic algebras. In order to do so we introduce O3-planes in the superstring description. We also find a brane realization for the mathematical map between two partitions of the same integer number known as collapse. Another result is that basic Kraft-Procesi transitions turn out to be described by the moduli space of orthosymplectic quivers with varying boundary conditions.

Exact supersymmetry on the lattice

NASA Astrophysics Data System (ADS)

Ghadab, Sofiane

We describe a new approach of putting supersymmetric theories on the lattice. The basic idea is to discretize a twisted formulation of the (extended) supersymmetric theory. One can think about the twisting as an exotic change of variables that modifies the quantum numbers of the original fields. It exposes a scalar nilpotent supercharge which one can be preserved exactly on the lattice. We give explicit examples from sigma models and Yang-Mills theories. For the former, we show how to deform the theory by the addition of potential terms which preserve the supersymmmetry and play the role of Wilson terms, thus preventing the appearance of doublers. For the Yang-Mills theories however, one can show that their twisted versions can be rewritten in terms of two real Kahler-Dirac fields whose components transform into each other under the twisted supersymmetry. Once written in this geometrical language, one can ensure that the model does not exhibit spectrum doubling if one maps the component tensor fields to appropriate geometrical structures in the lattice. Numerical study of the O(3) sigma models and U(2) and SU(2) Yang-Mills theories for the case N = D = 2 indicates that no additional fine tuning is needed to recover the continuum supersymmetric models.

Giant fields of the late 80s associated with type [open quotes]A[close quotes] subduction in South America

DOE Office of Scientific and Technical Information (OSTI.GOV)

Duval, B.; Cramez, C.; Figuera, J.

1993-02-01

About 10 billion bbl of recoverable oil have been found in these three fields for which the petroleum generating subsystem is very similar. The potential source rocks are the organic sediments associated with the major downlap surface of the post-Pangea continental encroachment sedimentary cycle, i.e., MFS 91, 5 Ma (La Luna formation). However, the concentrating physico-chemical petroleum subsystem is quite different. The El Furrial/Musipan field is associated with a Tertiary foredeep basin overlying a generating Atlantic type passive margin. On the other hand, Cusiana and Ceuta fields are associated with a Tertiary foredeep basin developed over a generating back-arc basin.more » The different stacking of sedimentary basins controls the migration/entrapment petroleum subsystem. In El Furrial/Musipan, decollement surfaces and their associated thrusts are predominant whereas, in Ceuta and Cusiana the majority of compressional structures are created by tectonic inversions. These tectonic settings create different petroleum systems: (a) supercharged with low impedance and lateral drainage in El Furrial/Musipan, (b) normally charged with high impedance and vertically drained in Ceuta and Cusiana area. Each case requires appropriated exploration approaches.« less

Emotional and rational product appeals in televised food advertisements for children: analysis of commercials shown on US broadcast networks.

PubMed

Page, Randy M; Brewster, Aaron

2007-12-01

The aggressive advertising and marketing of high caloric food products to children is implicated as a potential causative factor in the childhood obesity epidemic. This study analyzed 147 commercials appearing during children's programming on U.S. broadcast networks for a wide range of potential emotional and rational advertising appeals. The most prominent emotional appeals were fun/happiness and play followed by fantasy/ imagination, social enhancement/peer acceptance, and coolness/hipness. Many of the products used the term ;super-charged' or a similar adjective to describe the powerful taste or other physical properties of the product. More than one-third of all the commercials used a fruit appeal or association. Statements or depictions that a product was healthy or nutritious were quite rare among the commercials. This seems to imply that health and nutrition claims are understood by food marketers to not be salient concerns among children and as such are not a selling point to children. Commercials for high sugar cereal products and fast food restaurants differed in several respects. This study can serve to guide child health care professionals and other child advocates in designing measures that counter food advertising messages directed at children.

Increasing Protein Charge State When Using Laser Electrospray Mass Spectrometry

NASA Astrophysics Data System (ADS)

Karki, Santosh; Flanigan, Paul M.; Perez, Johnny J.; Archer, Jieutonne J.; Levis, Robert J.

2015-05-01

Femtosecond (fs) laser vaporization is used to transfer cytochrome c, myoglobin, lysozyme, and ubiquitin from the condensed phase into an electrospray (ES) plume consisting of a mixture of a supercharging reagent, m-nitrobenzyl alcohol ( m-NBA), and trifluoroacetic acid (TFA), acetic acid (AA), or formic acid (FA). Interaction of acid-sensitive proteins like cytochrome c and myoglobin with the highly charged ES droplets resulted in a shift to higher charge states in comparison with acid-stable proteins like lysozyme and ubiquitin. Laser electrospray mass spectrometry (LEMS) measurements showed an increase in both the average charge states (Zavg) and the charge state with maximum intensity (Zmode) for acid-sensitive proteins compared with conventional electrospray ionization mass spectrometry (ESI-MS) under equivalent solvent conditions. A marked increase in ion abundance of higher charge states was observed for LEMS in comparison with conventional electrospray for cytochrome c (ranging from 19+ to 21+ versus 13+ to 16+) and myoglobin (ranging from 19+ to 26+ versus 18+ to 21+) using an ES solution containing m-NBA and TFA. LEMS measurements as a function of electrospray flow rate yielded increasing charge states with decreasing flow rates for cytochrome c and myoglobin.

The problem of the turbo-compressor

NASA Technical Reports Server (NTRS)

Devillers, Rene

1920-01-01

In terminating the study of the adaptation of the engine to the airplane, we will examine the problem of the turbo-compressor,the first realization of which dates from the war; this will form an addition to the indications already given on supercharging at various altitudes. This subject is of great importance for the application of the turbo-compressor worked by the exhaust gases. As a matter of fact, a compressor increasing the pressure in the admission manifold may be controlled by the engine shaft by means of multiplication gear or by a turbine operated by the exhaust gas. Assuming that the increase of pressure in the admission manifold is the same in both cases, the pressure in the exhaust manifold would be greater in the case in which the compressor is worked by the exhaust gas and there would result a certain reduction of engine power which we must be able to calculate. On the other hand , if the compressor is controlled by the engine shaft, a certain fraction of the excess power supplied is utilized for the rotation of the compressor. In order to compare the two systems, it is there-fore necessary to determine the value of the reduction of power due to back pressure when the turbine is employed.

Diesel Combustion and Emission Using High Boost and High Injection Pressure in a Single Cylinder Engine

NASA Astrophysics Data System (ADS)

Aoyagi, Yuzo; Kunishima, Eiji; Asaumi, Yasuo; Aihara, Yoshiaki; Odaka, Matsuo; Goto, Yuichi

Heavy-duty diesel engines have adopted numerous technologies for clean emissions and low fuel consumption. Some are direct fuel injection combined with high injection pressure and adequate in-cylinder air motion, turbo-intercooler systems, and strong steel pistons. Using these technologies, diesel engines have achieved an extremely low CO2 emission as a prime mover. However, heavy-duty diesel engines with even lower NOx and PM emission levels are anticipated. This study achieved high-boost and lean diesel combustion using a single cylinder engine that provides good engine performance and clean exhaust emission. The experiment was done under conditions of intake air quantity up to five times that of a naturally aspirated (NA) engine and 200MPa injection pressure. The adopted pressure booster is an external supercharger that can control intake air temperature. In this engine, the maximum cylinder pressure was increased and new technologies were adopted, including a monotherm piston for endurance of Pmax =30MPa. Moreover, every engine part is newly designed. As the boost pressure increases, the rate of heat release resembles the injection rate and becomes sharper. The combustion and brake thermal efficiency are improved. This high boost and lean diesel combustion creates little smoke; ISCO and ISTHC without the ISNOx increase. It also yields good thermal efficiency.

The "Tokyo" consensus on propeller flaps.

PubMed

Pignatti, Marco; Ogawa, Rei; Hallock, Geoffrey G; Mateev, Musa; Georgescu, Alexandru V; Balakrishnan, Govindasamy; Ono, Shimpei; Cubison, Tania C S; D'Arpa, Salvatore; Koshima, Isao; Hyakusoku, Hikko

2011-02-01

Over the past few years, the use of propeller flaps, which base their blood supply on subcutaneous tissue or isolated perforators, has become increasingly popular. Because no consensus has yet been reached on terminology and nomenclature of the propeller flap, different and confusing uses of the term can be found in the literature. In this article, the authors report the consensus on the definition and classification of propeller flaps reached by the authors that gathered at the First Tokyo Meeting on Perforator and Propeller Flaps in June of 2009. Some peculiar aspects of the surgical technique are discussed. A propeller flap can be defined as an "island flap that reaches the recipient site through an axial rotation." The classification is based on the nourishing pedicle (subcutaneous pedicled propeller flap, perforator pedicled propeller flap, supercharged propeller flap), the degrees of skin island rotation (90 to 180 degrees) and, when possible, the artery of origin of the perforator. The propeller flap is a useful reconstructive tool that can achieve good cosmetic and functional results. A flap should be called a propeller flap only if it fulfils the definition above. The type of nourishing pedicle, the source vessel (when known), and the degree of skin island rotation should be specified for each flap.

Reporting from the Iceland Deep Drilling Project

NASA Astrophysics Data System (ADS)

Urban, Karl

2017-04-01

Geoscience-related topics are in many cases difficult to communicate to the public: Often they include dead soil which not easily tells lively stories. And it is hard to sell those topics to editors of public media. In addition the topics might also be politically supercharged if they are resource-related with a visible environmental impact. Therefore any researcher involved might be overcautious while talking to journalists. With a grant from the EGU Science Journalist Fellowship I travelled to Iceland in autumn 2016 to report about the Iceland Deep Drilling Project (IDDP). The project which started just weeks prior to my arrival aimed to drill the deepest borehole in a volcanically active region. During earlier trials the borehole collapsed or the drill string unintentionally hit magma. If successful the IDDP promises a much higher level of geothermal energy harvested. The IDDP was therefore ideally suited to be sold to public media outlets since Iceland's volcanic legacy easily tells a lively story. But the drilling's potential environmental impact makes it a political topic in Iceland - even though geothermal energy has a positive public perception. Therefore the IDDP included some pitfalls I observed several times before while reporting about geoscience research. Those could be circumvented if researchers and journalists knew better about their expectations before any interview takes place.

Use of supercharged cover screw as static magnetic field generator for bone healing, 1st part: in vitro enhancement of osteoblast-like cell differentiation.

PubMed

Bambini, F; Santarelli, A; Putignano, A; Procaccini, M; Orsini, G; Memè, L; Sartini, D; Emanuelli, M; Lo Muzio, L

2017-01-01

Since 1979, Pulsed electromagnetic fields (PEMFs) have been approved by the Food and Drug Administration as an effective method in the treatment of non-unions. As well as PEMFs, also static magnetic fields (SMFs) have been widely investigated in orthopaedic studies. Even if the exact mechanism of action is not well understood, a large number of studies showed specific effects both at cellular and tissue levels. As bone fracture healing and osseointegration share the same biological events, the application of magnetic field stimulation in order to facilitate the osseointegration process has been suggested. In this study we investigated the proliferation rate and gene expression profile of MG63 osteoblastic-like cells after a 24, 48 and 72-hour SMF stimulation, generated by a small, customized cover screw-shaped neodymium-iron-bore magnet placed in the inner cavity of a dental implant. As a result, we found that the application of a SMF to osteoblastic-like cells does slightly decrease cell proliferation rate while enhancing the expression of those genes correlated to differentiation and mineralization. Our findings represent, to our knowledge, the first clinical ready technique for dental implants showing the ability of SMF to promote the osteogenesis process in vitro.

Highly Reusable Space Transportation System Concept Evaluation (The Argus Launch Vehicle)

NASA Technical Reports Server (NTRS)

Olds, John R.; Bellini, Peter X.

1998-01-01

This paper summarizes the results of a conceptual design study that was performed in support of NASA's recent Highly Reusable Space Transportation study. The Argus concept uses a Maglifter magnetic-levitation sled launch assist system to accelerate it to a takeoff ground speed of 800 fps on its way to delivering a payload of 20,000 lb. to low earth orbit. Main propulsion is provided by two supercharged ejector rocket engines. The vehicle is autonomous and is fully reusable. A conceptual design exercise determined the vehicle gross weight to be approximately 597,250 lb. and the dry weight to be 75,500 lb. Aggressive weight and operations cost assumptions were used throughout the design process consistent with a second-generation reusable system that might be deployed in 10-15 years. Drawings, geometry, and weight of the concept are included. Preliminary development, production, and operations costs along with a business scenario assuming a price-elastic payload market are also included. A fleet of three Argus launch vehicles flying a total of 149 flights per year is shown to have a financial internal rate of return of 28%. At $169/lb., the recurring cost of Argus is shown to meet the study goal of $100/lb.-$200/lb., but optimum market price results in only a factor of two to five reduction compared to today's launch systems.

Impeller Creation at the Fabrication Shop

NASA Image and Video Library

1950-10-21

A mechanic and apprentice work on a wooden impeller in the Fabrication Shop at the NACA Lewis Flight Propulsion Laboratory. The 260-person Fabrication Division created almost all of the equipment and models used at the laboratory. The Technical Services Building, referred to as the “Fab Shop”, contained a number of specialized shops in the 1940s and 1950s. These included a Machine Shop, Sheet Metal Shop, Wood and Pattern Shop, Instrument Shop, Thermocouple Shop, Heat Treating Shop, Metallurgical Laboratory, and Fabrication Office. The Machine Shop fabricated research equipment not commercially available. During World War II these technicians produced high-speed cameras for combustion research, impellers and other supercharger components, and key equipment for the lab’s first supersonic wind tunnel. The Wood and Pattern Shop created everything from control panels and cabinets to aircraft model molds for sheet metal work. The Sheet Metal Shop had the ability to work with 0.01 to 4-inches thick steel plates. The Instrument Shop specialized in miniature parts and instrumentation, while the Thermocouple Shop standardized the installation of pitot tubes and thermocouples. The Metallurgical Laboratory contained a control lab for the Heat Treating Shop and a service lab for the NACA Lewis research divisions. The Heat Treating Shop heated metal parts to optimize their physical properties and contained a Precision Castings Foundry to manufacture equipment made of heat resisting alloys.

Cloning and characterization of a novel chondroitin sulfate/dermatan sulfate 4-O-endosulfatase from a marine bacterium.

PubMed

Wang, Wenshuang; Han, Wenjun; Cai, Xingya; Zheng, Xiaoyu; Sugahara, Kazuyuki; Li, Fuchuan

2015-03-20

Sulfatases are potentially useful tools for structure-function studies of glycosaminoglycans (GAGs). To date, various GAG exosulfatases have been identified in eukaryotes and prokaryotes. However, endosulfatases that act on GAGs have rarely been reported. Recently, a novel HA and CS lyase (HCLase) was identified for the first time from a marine bacterium (Han, W., Wang, W., Zhao, M., Sugahara, K., and Li, F. (2014) J. Biol. Chem. 289, 27886-27898). In this study, a putative sulfatase gene, closely linked to the hclase gene in the genome, was recombinantly expressed and characterized in detail. The recombinant protein showed a specific N-acetylgalactosamine-4-O-sulfatase activity that removes 4-O-sulfate from both disaccharides and polysaccharides of chondroitin sulfate (CS)/dermatan sulfate (DS), suggesting that this sulfatase represents a novel endosulfatase. The novel endosulfatase exhibited maximal reaction rate in a phosphate buffer (pH 8.0) at 30 °C and effectively removed 17-65% of 4-O-sulfates from various CS and DS and thus significantly inhibited the interactions of CS and DS with a positively supercharged fluorescent protein. Moreover, this endosulfatase significantly promoted the digestion of CS by HCLase, suggesting that it enhances the digestion of CS/DS by the bacterium. Therefore, this endosulfatase is a potential tool for use in CS/DS-related studies and applications. © 2015 by The American Society for Biochemistry and Molecular Biology, Inc.

The Use of Large Valve Overlap in Scavenging a Supercharged Spark-ignition Engine Using Fuel Injection

NASA Technical Reports Server (NTRS)

Schey, Oscar W; Young, Alfred W

1932-01-01

This investigation was conducted to determine the effect of more complete scavenging on the full throttle power and the fuel consumption of a four-stroke-cycle engine. The NACA single-cylinder universal test engine equipped with both a fuel-injection system and a carburetor was used. The engine was scavenged by using a large valve overlap and maintaining a pressure in the inlet manifold of 2 inches of mercury above atmospheric. The maximum valve overlap used was 112 degrees. Tests were conducted for a range of compression ratios from 5.5 to 8.5. Except for variable speed tests, all tests were conducted at an engine speed of 1,500 r.p.m. The results of the tests show that the clearance volume of an engine can be scavenged by using a large valve overlap and about 2 to 5 inches of mercury pressure difference between the inlet and exhaust valve. With a fuel-injection system when the clearance volume was scavenged, a b.m.e.p. of over 185 pounds per square inch and a fuel consumption of 9.45 pound per brake horsepower per hour were obtained with a 6.5 compression ratio. An increase of approximately 10 pounds per square inch b.m.e.p. was obtained with a fuel-injection system over that with a carburetor.

The Combination of Internal-Combustion Engine and Gas Turbine

NASA Technical Reports Server (NTRS)

Zinner, K.

1947-01-01

While the gas turbine by itself has been applied in particular cases for power generation and is in a state of promising development in this field, it has already met with considerable success in two cases when used as an exhaust turbine in connection with a centrifugal compressor, namely, in the supercharging of combustion engines and in the Velox process, which is of particular application for furnaces. In the present paper the most important possibilities of combining a combustion engine with a gas turbine are considered. These "combination engines " are compared with the simple gas turbine on whose state of development a brief review will first be given. The critical evaluation of the possibilities of development and fields of application of the various combustion engine systems, wherever it is not clearly expressed in the publications referred to, represents the opinion of the author. The state of development of the internal-combustion engine is in its main features generally known. It is used predominantly at the present time for the propulsion of aircraft and road vehicles and, except for certain restrictions due to war conditions, has been used to an increasing extent in ships and rail cars and in some fields applied as stationary power generators. In the Diesel engine a most economical heat engine with a useful efficiency of about 40 percent exists and in the Otto aircraft engine a heat engine of greatest power per unit weight of about 0.5 kilogram per horsepower.

Rubisco activity and regulation as targets for crop improvement.

PubMed

Parry, Martin A J; Andralojc, P John; Scales, Joanna C; Salvucci, Michael E; Carmo-Silva, A Elizabete; Alonso, Hernan; Whitney, Spencer M

2013-01-01

Rubisco (ribulose-1,5-bisphosphate (RuBP) carboxylase/oxygenase) enables net carbon fixation through the carboxylation of RuBP. However, some characteristics of Rubisco make it surprisingly inefficient and compromise photosynthetic productivity. For example, Rubisco catalyses a wasteful reaction with oxygen that leads to the release of previously fixed CO(2) and NH(3) and the consumption of energy during photorespiration. Furthermore, Rubisco is slow and large amounts are needed to support adequate photosynthetic rates. Consequently, Rubisco has been studied intensively as a prime target for manipulations to 'supercharge' photosynthesis and improve both productivity and resource use efficiency. The catalytic properties of Rubiscos from diverse sources vary considerably, suggesting that changes in turnover rate, affinity, or specificity for CO(2) can be introduced to improve Rubisco performance in specific crops and environments. While attempts to manipulate plant Rubisco by nuclear transformation have had limited success, modifying its catalysis by targeted changes to its catalytic large subunit via chloroplast transformation have been much more successful. However, this technique is still in need of development for most major food crops including maize, wheat, and rice. Other bioengineering approaches for improving Rubisco performance include improving the activity of its ancillary protein, Rubisco activase, in addition to modulating the synthesis and degradation of Rubisco's inhibitory sugar phosphate ligands. As the rate-limiting step in carbon assimilation, even modest improvements in the overall performance of Rubisco pose a viable pathway for obtaining significant gains in plant yield, particularly under stressful environmental conditions.

High Ethanol Fuel Endurance: A Study of the Effects of Running Gasoline with 15% Ethanol Concentration in Current Production Outboard Four-Stroke Engines and Conventional Two-Stroke Outboard Marine Engines

DOE Office of Scientific and Technical Information (OSTI.GOV)

Hilbert, D.

2011-10-01

Three Mercury Marine outboard marine engines were evaluated for durability using E15 fuel -- gasoline blended with 15% ethanol. Direct comparison was made to operation on E0 (ethanol-free gasoline) to determine the effects of increased ethanol on engine durability. Testing was conducted using a 300-hour wide-open throttle (WOT) test protocol, a typical durability cycle used by the outboard marine industry. Use of E15 resulted in reduced CO emissions, as expected for open-loop, non-feedback control engines. HC emissions effects were variable. Exhaust gas and engine operating temperatures increased as a consequence of leaner operation. Each E15 test engine exhibited some deteriorationmore » that may have been related to the test fuel. The 9.9 HP, four-stroke E15 engine exhibited variable hydrocarbon emissions at 300 hours -- an indication of lean misfire. The 300HP, four-stroke, supercharged Verado engine and the 200HP, two-stroke legacy engine tested with E15 fuel failed to complete the durability test. The Verado engine failed three exhaust valves at 285 endurance hours while the 200HP legacy engine failed a main crank bearing at 256 endurance hours. All E0-dedicated engines completed the durability cycle without incident. Additional testing is necessary to link the observed engine failures to ethanol in the test fuel.« less

Combining genetic and evolutionary engineering to establish C4 metabolism in C3 plants.

PubMed

Li, Yuanyuan; Heckmann, David; Lercher, Martin J; Maurino, Veronica G

2017-01-01

To feed a world population projected to reach 9 billion people by 2050, the productivity of major crops must be increased by at least 50%. One potential route to boost the productivity of cereals is to equip them genetically with the 'supercharged' C 4 type of photosynthesis; however, the necessary genetic modifications are not sufficiently understood for the corresponding genetic engineering programme. In this opinion paper, we discuss a strategy to solve this problem by developing a new paradigm for plant breeding. We propose combining the bioengineering of well-understood traits with subsequent evolutionary engineering, i.e. mutagenesis and artificial selection. An existing mathematical model of C 3 -C 4 evolution is used to choose the most promising path towards this goal. Based on biomathematical simulations, we engineer Arabidopsis thaliana plants that express the central carbon-fixing enzyme Rubisco only in bundle sheath cells (Ru-BSC plants), the localization characteristic for C 4 plants. This modification will initially be deleterious, forcing the Ru-BSC plants into a fitness valley from where previously inaccessible adaptive steps towards C 4 photosynthesis become accessible through fitness-enhancing mutations. Mutagenized Ru-BSC plants are then screened for improved photosynthesis, and are expected to respond to imposed artificial selection pressures by evolving towards C 4 anatomy and biochemistry. © The Author 2016. Published by Oxford University Press on behalf of the Society for Experimental Biology. All rights reserved. For permissions, please email: journals.permissions@oup.com.

Direct characterization of the native structure and mechanics of cyanobacterial carboxysomes.

PubMed

Faulkner, Matthew; Rodriguez-Ramos, Jorge; Dykes, Gregory F; Owen, Siân V; Casella, Selene; Simpson, Deborah M; Beynon, Robert J; Liu, Lu-Ning

2017-08-03

Carboxysomes are proteinaceous organelles that play essential roles in enhancing carbon fixation in cyanobacteria and some proteobacteria. These self-assembling organelles encapsulate Ribulose 1,5-bisphosphate carboxylase/oxygenase (Rubisco) and carbonic anhydrase using a protein shell structurally resembling an icosahedral viral capsid. The protein shell serves as a physical barrier to protect enzymes from the cytosol and a selectively permeable membrane to mediate transport of enzyme substrates and products. The structural and mechanical nature of native carboxysomes remain unclear. Here, we isolate functional β-carboxysomes from the cyanobacterium Synechococcus elongatus PCC7942 and perform the first characterization of the macromolecular architecture and inherent physical mechanics of single β-carboxysomes using electron microscopy, atomic force microscopy (AFM) and proteomics. Our results illustrate that the intact β-carboxysome comprises three structural domains, a single-layered icosahedral shell, an inner layer and paracrystalline arrays of interior Rubisco. We also observe the protein organization of the shell and partial β-carboxysomes that likely serve as the β-carboxysome assembly intermediates. Furthermore, the topography and intrinsic mechanics of functional β-carboxysomes are determined in native conditions using AFM and AFM-based nanoindentation, revealing the flexible organization and soft mechanical properties of β-carboxysomes compared to rigid viruses. Our study provides new insights into the natural characteristics of β-carboxysome organization and nanomechanics, which can be extended to diverse bacterial microcompartments and are important considerations for the design and engineering of functional carboxysomes in other organisms to supercharge photosynthesis. It offers an approach for inspecting the structural and mechanical features of synthetic metabolic organelles and protein scaffolds in bioengineering.

Performance of a Fuel-Cell-Powered, Small Electric Airplane Assessed

NASA Technical Reports Server (NTRS)

Berton, Jeffrey J.

2004-01-01

Rapidly emerging fuel-cell-power technologies may be used to launch a new revolution of electric propulsion systems for light aircraft. Future small electric airplanes using fuel cell technologies hold the promise of high reliability, low maintenance, low noise, and - with the exception of water vapor - zero emissions. An analytical feasibility and performance assessment was conducted by NASA Glenn Research Center's Airbreathing Systems Analysis Office of a fuel-cell-powered, propeller-driven, small electric airplane based on a model of the MCR-01 two-place kitplane (Dyn'Aero, Darois, France). This assessment was conducted in parallel with an ongoing effort by the Advanced Technology Products Corporation and the Foundation for Advancing Science and Technology Education. Their project - partially funded by a NASA grant - is to design, build, and fly the first manned, continuously propelled, nongliding electric airplane. In our study, an analytical performance model of a proton exchange membrane (PEM) fuel cell propulsion system was developed and applied to a notional, two-place light airplane modeled after the MCR-01 kitplane. The PEM fuel cell stack was fed pure hydrogen fuel and humidified ambient air via a small automotive centrifugal supercharger. The fuel cell performance models were based on chemical reaction analyses calibrated with published data from the fledgling U.S. automotive fuel cell industry. Electric propeller motors, rated at two shaft power levels in separate assessments, were used to directly drive a two-bladed, variable-pitch propeller. Fuel sources considered were compressed hydrogen gas and cryogenic liquid hydrogen. Both of these fuel sources provided pure, contaminant-free hydrogen for the PEM cells.

Serverification of Molecular Modeling Applications: The Rosetta Online Server That Includes Everyone (ROSIE)

PubMed Central

Conchúir, Shane Ó.; Der, Bryan S.; Drew, Kevin; Kuroda, Daisuke; Xu, Jianqing; Weitzner, Brian D.; Renfrew, P. Douglas; Sripakdeevong, Parin; Borgo, Benjamin; Havranek, James J.; Kuhlman, Brian; Kortemme, Tanja; Bonneau, Richard; Gray, Jeffrey J.; Das, Rhiju

2013-01-01

The Rosetta molecular modeling software package provides experimentally tested and rapidly evolving tools for the 3D structure prediction and high-resolution design of proteins, nucleic acids, and a growing number of non-natural polymers. Despite its free availability to academic users and improving documentation, use of Rosetta has largely remained confined to developers and their immediate collaborators due to the code’s difficulty of use, the requirement for large computational resources, and the unavailability of servers for most of the Rosetta applications. Here, we present a unified web framework for Rosetta applications called ROSIE (Rosetta Online Server that Includes Everyone). ROSIE provides (a) a common user interface for Rosetta protocols, (b) a stable application programming interface for developers to add additional protocols, (c) a flexible back-end to allow leveraging of computer cluster resources shared by RosettaCommons member institutions, and (d) centralized administration by the RosettaCommons to ensure continuous maintenance. This paper describes the ROSIE server infrastructure, a step-by-step ‘serverification’ protocol for use by Rosetta developers, and the deployment of the first nine ROSIE applications by six separate developer teams: Docking, RNA de novo, ERRASER, Antibody, Sequence Tolerance, Supercharge, Beta peptide design, NCBB design, and VIP redesign. As illustrated by the number and diversity of these applications, ROSIE offers a general and speedy paradigm for serverification of Rosetta applications that incurs negligible cost to developers and lowers barriers to Rosetta use for the broader biological community. ROSIE is available at http://rosie.rosettacommons.org. PMID:23717507

Knock-Limited Performance of Triptane and 28-R Fuel Blends as Affected by Changes in Compression Ratio and in Engine Operating Variables

NASA Technical Reports Server (NTRS)

Brun, Rinaldo J.; Feder, Melvin S.; Fisher, William F.

1947-01-01

A knock-limited performance investigation was conducted on blends of triptane and 28-P fuel with a 12-cylinder, V-type, liquid-cooled aircraft engine of 1710-cubic-inch displacement at three compression ratios: 6.65, 7.93, and 9.68. At each compression ratio, the effect of changes in temperature of the inlet air to the auxiliary-stage supercharger and in fuel-air ratio were investigated at engine speeds of 2280 and. 3000 rpm. The results show that knock-limited engine performance, as improved by the use of triptane, allowed operation at both take-off and cruising power at a compression ratio of 9.68. At an inlet-air temperature of 60 deg F, an engine speed of 3000 rpm ; and a fuel-air ratio of 0,095 (approximately take-off conditions), a knock-limited engine output of 1500 brake horsepower was possible with 100-percent 28-R fuel at a compression ratio of 6.65; 20-percent triptane was required for the same power output at a compression ratio of 7.93, and 75 percent at a compression ratio of 9.68 allowed an output of 1480 brake horsepower. Knock-limited power output was more sensitive to changes in fuel-air ratio as the engine speed was increased from 2280 to 3000 rpm, as the compression ratio is raised from 6.65 to 9.68, or as the inlet-air temperature is raised from 0 deg to 120 deg F.

Expression of Functional Human Sialyltransferases ST3Gal1 and ST6Gal1 in Escherichia coli

PubMed Central

Ortiz-Soto, Maria Elena; Seibel, Jürgen

2016-01-01

Sialyltransferases (STs) are disulfide-containing, type II transmembrane glycoproteins that catalyze the transfer of sialic acid to proteins and lipids and participate in the synthesis of the core structure oligosaccharides of human milk. Sialic acids are found at the outermost position of glycostructures, playing a key role in health and disease. Sialylation is also essential for the production of recombinant therapeutic proteins (RTPs). Despite their importance, availability of sialyltransferases is limited due to the low levels of stable, soluble and active protein produced in bacterial expression systems, which hampers biochemical and structural studies on these enzymes and restricts biotechnological applications. We report the successful expression of active human sialyltransferases ST3Gal1 and ST6Gal1 in commercial Escherichia coli strains designed for production of disulfide-containing proteins. Fusion of hST3Gal1 with different solubility enhancers and substitution of exposed hydrophobic amino acids by negatively charged residues (supercharging-like approach) were performed to promote solubility and folding. Co-expression of sialyltransferases with the chaperon/foldases sulfhydryl oxidase, protein disulfide isomerase and disulfide isomerase C was explored to improve the formation of native disulfide bonds. Active sialyltransferases fused with maltose binding protein (MBP) were obtained in sufficient amounts for biochemical and structural studies when expressed under oxidative conditions and co-expression of folding factors increased the yields of active and properly folded sialyltransferases by 20%. Mutation of exposed hydrophobic amino acids increased recovery of active enzyme by 2.5-fold, yielding about 7 mg of purified protein per liter culture. Functionality of recombinant enzymes was evaluated in the synthesis of sialosides from the β-d-galactoside substrates lactose, N-acetyllactosamine and benzyl 2-acetamido-2-deoxy-3-O-(β-d-galactopyranosyl)-α-d-galactopyranoside. PMID:27166796

Progress in energy generation for Canadian remote sites

NASA Astrophysics Data System (ADS)

Saad, Y.; Younes, R.; Abboudi, S.; Ilinca, A.; Nohra, C.

2016-07-01

Many remote areas around the world are isolated, for various reasons, from electricity networks. They are usually supplied with electricity through diesel generators. The cost of operation and transportation of diesel fuel in addition to its price have led to the procurement of a more efficient and environmentally greener method of supply. Various studies have shown that a wind-diesel hybrid system with compressed air storage (WDCAS) seems to be one of the best solutions, and presents itself as an optimal configuration for the electrification of isolated sites. This system allows significant fuel savings to be made because the stored compressed air is used to supercharge the engine. In order to optimize system performance and minimize fuel consumption, installation of a system for recovering and storing the heat of compression (TES) seems necessary. In addition, the use of hydro-pneumatic energy storage systems that use the same machine as the hydraulic pump and turbine allow us to store energy in tight spaces and, if possible, contribute to power generation. The scrupulous study of this technical approach will be the focus of our research which will validate (or not) the use of such a system for the regulation of frequency of electrical networks. In this article we will skim through the main research that recently examined the wind-diesel hybrid system which addressed topics such as adiabatic compression and hydro-pneumatic storage. Instead, we will offer (based on existing studies) a new ACP-WDCAS (wind-diesel hybrid system with adiabatic air compression and storage at constant pressure), which combines these three concepts in one system for the optimization of wind-diesel hybrid system.

Can increased leaf photosynthesis be converted into higher crop mass production? A simulation study for rice using the crop model GECROS

PubMed Central

Struik, Paul C.

2017-01-01

Abstract Various genetic engineering routes to enhance C3 leaf photosynthesis have been proposed to improve crop productivity. However, their potential contribution to crop productivity needs to be assessed under realistic field conditions. Using 31 year weather data, we ran the crop model GECROS for rice in tropical, subtropical, and temperate environments, to evaluate the following routes: (1) improving mesophyll conductance (gm); (2) improving Rubisco specificity (Sc/o); (3) improving both gm and Sc/o; (4) introducing C4 biochemistry; (5) introducing C4 Kranz anatomy that effectively minimizes CO2 leakage; (6) engineering the complete C4 mechanism; (7) engineering cyanobacterial bicarbonate transporters; (8) engineering a more elaborate cyanobacterial CO2-concentrating mechanism (CCM) with the carboxysome in the chloroplast; and (9) a mechanism that combines the low ATP cost of the cyanobacterial CCM and the high photosynthetic capacity per unit leaf nitrogen. All routes improved crop mass production, but benefits from Routes 1, 2, and 7 were ≤10%. Benefits were higher in the presence than in the absence of drought, and under the present climate than for the climate predicted for 2050. Simulated crop mass differences resulted not only from the increased canopy photosynthesis competence but also from changes in traits such as light interception and crop senescence. The route combinations gave larger effects than the sum of the effects of the single routes, but only Route 9 could bring an advantage of ≥50% under any environmental conditions. To supercharge crop productivity, exploring a combination of routes in improving the CCM, photosynthetic capacity, and quantum efficiency is required. PMID:28379522

Fat necrosis in autologous abdomen-based breast reconstruction: a systematic review.

PubMed

Khansa, Ibrahim; Momoh, Adeyiza O; Patel, Priti P; Nguyen, John T; Miller, Michael J; Lee, Bernard T

2013-03-01

Fat necrosis is a common and potentially exasperating complication of autologous breast reconstruction. The authors performed a systematic review of the English literature on autologous breast reconstruction to determine significant patient and surgical factors that are predictors of postoperative fat necrosis. A PubMed search using the terms "fat necrosis" and "breast reconstruction" was conducted. Articles were screened using predetermined inclusion and exclusion criteria. Data collected included patient characteristics, reconstructive techniques used, and the specific postoperative morbidity of interest. Patient cohorts were pooled, and the incidence of fat necrosis was calculated in the presence and absence of each risk factor. Chi-square analysis was applied, and p < 0.05 was considered statistically significant. Of 172 articles found, 70 met the inclusion criteria. The mean rate of fat necrosis was 11.3 percent. Deep inferior epigastric artery perforator flaps had the highest rate of fat necrosis (14.4 percent), followed by pedicled transverse rectus abdominis musculocutaneous (12.3 percent), superficial inferior epigastric artery (8.1 percent), and free transverse rectus abdominis musculocutaneous flaps (6.9 percent). Significant predictors of fat necrosis included obesity (p = 0.035), prereconstruction irradiation (p = 0.022), postreconstruction irradiation (p < 0.001), active smoking (p < 0.001), and abdominal scars (p = 0.05). Protective factors included supercharging (p < 0.001) and bilateral reconstruction (p = 0.01). Although there is little agreement in the literature regarding risk factors for fat necrosis, the authors were able to demonstrate several significant predictors by systematically analyzing 70 articles. Improved knowledge of the risk factors for fat necrosis can help surgeons provide improved preoperative counseling and take measures to minimize the risk of this complication.

Supraclavicular artery perforator flap in management of post-burn neck reconstruction: clinical experience

PubMed Central

Ismail, H.; Elshobaky, A.

2016-01-01

Summary Anterior cervical contractures of the neck represent a great challenge for plastic and reconstructive surgeons. Necks can be reconstructed with a wide range of surgical techniques, including chimeric flaps, supercharged flap, pre-expanded flaps, “superthin” flaps and perforator flaps. The supraclavicular flap is easy to harvest without the need for free tissue transfer. It provides a relatively large flap for neck resurfacing with tissue very similar to that of the neck. Between January 2013 and March 2015, 20 patients suffering from postburn neck contracture underwent reconstruction with 20 unilateral supraclavicular artery perforator flaps. Nineteen patients had post-burn neck contractures (9 cases type Іc, 10 cases type Пc) while only one had post-burn granulation tissue in the neck. We harvested fifteen flaps from the right side and five from the left. Size of the reconstructed defect ranged from 23x10 to14x6, and flap size varied from 25/11 to 16/7cm. Period of follow up ranged from 27-2months (average 12.3). Nineteen flaps survived well (95% survival rate): only one was lost due to iatrogenic extensive dissection over the pedicle. Five cases showed distal superficial epidermolysis, and 2 cases showed 2 cm complete distal necrosis. All patients were managed conservatively. Our results coincide with other literature results confirming the efficacy and rich vascularity of this flap. In all cases with distal partial necrosis, flaps were 23 cm or more. We recommend that supraclavicular flaps of more than 22 cm in length are not harvested immediately and that flaps are expanded before harvesting. Expanding the supraclavicular flap increases its surface area and decreases donor site morbidity. PMID:28149252

Protein charge distribution in proteomes and its impact on translation

PubMed Central

Requião, Rodrigo D.; Fernandes, Luiza; de Souza, Henrique José Araujo; Rossetto, Silvana; Domitrovic, Tatiana

2017-01-01

As proteins are synthesized, the nascent polypeptide must pass through a negatively charged exit tunnel. During this stage, positively charged stretches can interact with the ribosome walls and slow the translation. Therefore, charged polypeptides may be important factors that affect protein expression. To determine the frequency and distribution of positively and negatively charged stretches in different proteomes, the net charge was calculated for every 30 consecutive amino acid residues, which corresponds to the length of the ribosome exit tunnel. The following annotated and reviewed proteins in the UniProt database (Swiss-Prot) were analyzed: 551,705 proteins from different organisms and a total of 180 million protein segments. We observed that there were more negative than positive stretches and that super-charged positive sequences (i.e., net charges ≥ 14) were underrepresented in the proteomes. Overall, the proteins were more positively charged at their N-termini and C-termini, and this feature was present in most organisms and subcellular localizations. To investigate whether the N-terminal charges affect the elongation rates, previously published ribosomal profiling data obtained from S. cerevisiae, without translation-interfering drugs, were analyzed. We observed a nonlinear effect of the charge on the ribosome occupancy in which values ≥ +5 and ≤ -6 showed increased and reduced ribosome densities, respectively. These groups also showed different distributions across 80S monosomes and polysomes. Basic polypeptides are more common within short proteins that are translated by monosomes, whereas negative stretches are more abundant in polysome-translated proteins. These findings suggest that the nascent peptide charge impacts translation and can be one of the factors that regulate translation efficiency and protein expression. PMID:28531225

Thermophilic Ferritin: Versatile Nanohost

NASA Astrophysics Data System (ADS)

Pulsipher, Katherine W.

Thermophilic ferritin from Archaeoglobus fulgidus (AfFtn) is a 24meric, hollow, cage-like protein, whose native function is the oxidation, mineralization, and storage of iron. Unique among ferritins, its self-assembly is dependent on high ionic strength, reflecting the deep sea thermal vent environment where A. fulgidus is found. This ionic strength dependence can be used to encapsulate charged cargo within the AfFtn cavity. Its subunits self-assemble into tetrahedral symmetry, resulting in four, large (4.5 nm), triangular pores, not found in other ferritins. Due to its size (12 nm outer diameter, 8 nm inner diameter), self-assembly properties, and potential for both genetic and chemical modification, AfFtn is an ideal nanocontainer for a variety of cargo, including inorganic nanoparticles and proteins. We have sought to better understand the self-assembly of AfFtn and its encapsulation of various cargo. Guided by computational analysis and through mutagenesis, we have investigated the role of electrostatics along the AfFtn trimeric interface in self-assembly. We have developed a series of single point mutants with increasingly favorable cage assembly. One specific mutation, E65R, has a dramatic effect on AfFtn, almost entirely preventing disassembly and enhancing thermal stability by 14°C. By using a novel graphene-based microelectrode, we have determined that AfFtn maintains its quaternary structure upon encapsulation of a gold nanoparticle, developing a new tool for investigating protein-nanomaterial interactions. We have also shown that AfFtn can be used to template seeded gold nanoparticle growth and have explored two often neglected factors in ferritin-nanoparticle templating: the charge of the gold salt used, and the size of the protein pores. Our results demonstrate that the open, porous structure of AfFtn allows more efficient particle growth than typical closed-pore ferritins. Finally, we have expanded the cargo uptake of AfFtn beyond nanoparticles to include proteins, encapsulating supercharged GFP. The AfFtn-cargo complexes developed here have application in catalysis, nanomaterials synthesis, and targeted delivery.

Heterotic supergravity with internal almost-Kähler spaces; instantons for SO(32), or E 8 × E 8, gauge groups; and deformed black holes with soliton, quasiperiodic and/or pattern-forming structures

NASA Astrophysics Data System (ADS)

Bubuianu, Laurenţiu; Irwin, Klee; Vacaru, Sergiu I.

2017-04-01

Heterotic supergravity with (1  +  3)-dimensional domain wall configurations and (warped) internal, six dimensional, almost-Kähler manifolds {{}6}\\text{X} are studied. Considering ten dimensional spacetimes with nonholonomic distributions and conventional double fibrations, 2  +  2  +  ...  =  2  +  2  +  3  +  3, and associated SU(3) structures on internal space, we generalize for real, internal, almost symplectic gravitational structures the constructions with gravitational and gauge instantons of tanh-kink type [1, 2]. They include the first {α\\prime} corrections to the heterotic supergravity action, parameterized in a form to imply nonholonomic deformations of the Yang-Mills sector and corresponding Bianchi identities. We show how it is possible to construct a variety of solutions depending on the type of nonholonomic distributions and deformations of ‘prime’ instanton configurations characterized by two real supercharges. This corresponds to N=1/2 supersymmetric, nonholonomic manifolds from the four dimensional point of view. Our method provides a unified description of embedding nonholonomically deformed tanh-kink-type instantons into half-BPS solutions of heterotic supergravity. This allows us to elaborate new geometric methods of constructing exact solutions of motion equations, with first order {α\\prime} corrections to the heterotic supergravity. Such a formalism is applied for general and/or warped almost-Kähler configurations, which allows us to generate nontrivial (1  +  3)-d domain walls and black hole deformations determined by quasiperiodic internal space structures. This formalism is utilized in our associated publication [3] in order to construct and study generic off-diagonal nonholonomic deformations of the Kerr metric, encoding contributions from heterotic supergravity.

Asymptotic structure of N=2 supergravity in 3D: extended super-BMS3 and nonlinear energy bounds

NASA Astrophysics Data System (ADS)

Fuentealba, Oscar; Matulich, Javier; Troncoso, Ricardo

2017-09-01

The asymptotically flat structure of N=(2,0) supergravity in three spacetime dimensions is explored. The asymptotic symmetries are found to be spanned by an extension of the super-BMS3 algebra, endowed with two independent affine û(1) currents of electric and magnetic type. These currents are associated to U(1) fields being even and odd under parity, respectively. Remarkably, although the U(1) fields do not generate a backreaction on the metric, they provide nontrivial Sugawara-like contributions to the BMS3 generators, and hence to the energy and the angular momentum. Consequently, the entropy of flat cosmological spacetimes endowed with U(1) fields acquires a nontrivial dependence on the zero modes of the û(1) charges. If the spin structure is odd, the ground state corresponds to Minkowski spacetime, and although the anticommutator of the canonical supercharges is linear in the energy and in the electric-like û(1) charge, the energy becomes bounded from below by the energy of the ground state shifted by the square of the electric-like û(1) charge. If the spin structure is even, the same bound for the energy generically holds, unless the absolute value of the electric-like charge is less than minus the mass of Minkowski spacetime in vacuum, so that the energy has to be nonnegative. The explicit form of the global and asymptotic Killing spinors is found for a wide class of configurations that fulfills our boundary conditions, and they exist precisely when the corresponding bounds are saturated. It is also shown that the spectra with periodic or antiperiodic boundary conditions for the fermionic fields are related by spectral flow, in a similar way as it occurs for the N=2 super-Virasoro algebra. Indeed, our supersymmetric extension of BMS3 can be recovered from the Inönü-Wigner contraction of the superconformal algebra with N=(2,2) , once the fermionic generators of the right copy are truncated.

The Sun-Earth connect 2: Modelling patterns of a fractal Sun in time and space using the fine structure constant

NASA Astrophysics Data System (ADS)

Baker, Robert G. V.

2017-02-01

Self-similar matrices of the fine structure constant of solar electromagnetic force and its inverse, multiplied by the Carrington synodic rotation, have been previously shown to account for at least 98% of the top one hundred significant frequencies and periodicities observed in the ACRIM composite irradiance satellite measurement and the terrestrial 10.7cm Penticton Adjusted Daily Flux data sets. This self-similarity allows for the development of a time-space differential equation (DE) where the solutions define a solar model for transmissions through the core, radiative, tachocline, convective and coronal zones with some encouraging empirical and theoretical results. The DE assumes a fundamental complex oscillation in the solar core and that time at the tachocline is smeared with real and imaginary constructs. The resulting solutions simulate for tachocline transmission, the solar cycle where time-line trajectories either 'loop' as Hermite polynomials for an active Sun or 'tail' as complementary error functions for a passive Sun. Further, a mechanism that allows for the stable energy transmission through the tachocline is explored and the model predicts the initial exponential coronal heating from nanoflare supercharging. The twisting of the field at the tachocline is then described as a quaternion within which neutrinos can oscillate. The resulting fractal bubbles are simulated as a Julia Set which can then aggregate from nanoflares into solar flares and prominences. Empirical examples demonstrate that time and space fractals are important constructs in understanding the behaviour of the Sun, from the impact on climate and biological histories on Earth, to the fractal influence on the spatial distributions of the solar system. The research suggests that there is a fractal clock underpinning solar frequencies in packages defined by the fine structure constant, where magnetic flipping and irradiance fluctuations at phase changes, have periodically impacted on the Earth and the rest of the solar system since time immemorial.

Numerical analysis of flow interaction of turbine system in two-stage turbocharger of internal combustion engine

NASA Astrophysics Data System (ADS)

Liu, Y. B.; Zhuge, W. L.; Zhang, Y. J.; Zhang, S. Y.

2016-05-01

To reach the goal of energy conservation and emission reduction, high intake pressure is needed to meet the demand of high power density and high EGR rate for internal combustion engine. Present power density of diesel engine has reached 90KW/L and intake pressure ratio needed is over 5. Two-stage turbocharging system is an effective way to realize high compression ratio. Because turbocharging system compression work derives from exhaust gas energy. Efficiency of exhaust gas energy influenced by design and matching of turbine system is important to performance of high supercharging engine. Conventional turbine system is assembled by single-stage turbocharger turbines and turbine matching is based on turbine MAP measured on test rig. Flow between turbine system is assumed uniform and value of outlet physical quantities of turbine are regarded as the same as ambient value. However, there are three-dimension flow field distortion and outlet physical quantities value change which will influence performance of turbine system as were demonstrated by some studies. For engine equipped with two-stage turbocharging system, optimization of turbine system design will increase efficiency of exhaust gas energy and thereby increase engine power density. However flow interaction of turbine system will change flow in turbine and influence turbine performance. To recognize the interaction characteristics between high pressure turbine and low pressure turbine, flow in turbine system is modeled and simulated numerically. The calculation results suggested that static pressure field at inlet to low pressure turbine increases back pressure of high pressure turbine, however efficiency of high pressure turbine changes little; distorted velocity field at outlet to high pressure turbine results in swirl at inlet to low pressure turbine. Clockwise swirl results in large negative angle of attack at inlet to rotor which causes flow loss in turbine impeller passages and decreases turbine efficiency. However negative angle of attack decreases when inlet swirl is anti-clockwise and efficiency of low pressure turbine can be increased by 3% compared to inlet condition of clockwise swirl. Consequently flow simulation and analysis are able to aid in figuring out interaction mechanism of turbine system and optimizing turbine system design.

Development and Testing of a 6-Cylinder HCCI Engine for Distributed Generation

DOE Office of Scientific and Technical Information (OSTI.GOV)

Flowers, D L; Martinez-Frias, J; Espinosa-Loza, F

2005-07-12

This paper describes the technical approach for converting a Caterpillar 3406 natural gas spark ignited engine into HCCI mode. The paper describes all stages of the process, starting with a preliminary analysis that determined that the engine can be operated by preheating the intake air with a heat exchanger that recovers energy from the exhaust gases. This heat exchanger plays a dual role, since it is also used for starting the engine. For start-up, the heat exchanger is preheated with a natural gas burner. The engine is therefore started in HCCI mode, avoiding the need to handle the potentially difficultmore » transition from SI or diesel mode to HCCI. The fueling system was modified by replacing the natural gas carburetor with a liquid petroleum gas (LPG) carburetor. This modification sets an upper limit for the equivalence ratio at {phi} {approx} 0.4, which is ideal for HCCI operation and guarantees that the engine will not fail due to knock. Equivalence ratio can be reduced below 0.4 for low load operation with an electronic control valve. Intake boosting has been a challenge, as commercially available turbochargers are not a good match for the engine, due to the low HCCI exhaust temperature. Commercial introduction of HCCI engines for stationary power will therefore require the development of turbochargers designed specifically for this mode of operation. Considering that no appropriate off-the-shelf turbocharger for HCCI engines exists at this time, we are investigating mechanical supercharging options, which will deliver the required boost pressure (3 bar absolute intake) at the expense of some reduction in the output power and efficiency. An appropriate turbocharger can later be installed for improved performance when it becomes available or when a custom turbocharger is developed. The engine is now running in HCCI mode and producing power in an essentially naturally aspirated mode. Current work focuses on developing an automatic controller for obtaining consistent combustion in the 6 cylinders. The engine will then be tested for 1000 hours to demonstrate durability. This paper presents intermediate progress towards development of an HCCI engine for stationary power generation and next steps towards achieving the project goals.« less

Department of Energy. Jobs and Innovation Accelerator Challenge (JIAC) Program

DOE Office of Scientific and Technical Information (OSTI.GOV)

Riley, Jon

1.1 NCMS Digital Manufacturing Initiative The people and businesses of Southeast Michigan have long been known for their prowess in the automotive industry, a sector built on the innovation of the assembly line and the rise of mass production as a manufacturing model. Just as the assembly line was the key to a strong manufacturing base a century ago, a digital manufacturing infrastructure is critical to the future of industry. Economic uncertainty has slowed innovation, but access to cutting-edge tools such as high performance modeling, simulation and analysis (MSA) provides a bold path forward, ensuring global competitiveness and transforming ourmore » manufacturing processes. Digital manufacturing is, essentially, the virtualization of processes that had been physical. Many larger manufacturers have embraced it, but the majority of small and medium-sized manufacturers (SMMs) have not. The Digital Manufacturing Initiative is a bold, national effort by the National Center for Manufacturing Sciences (NCMS) to put manufacturing innovation on fast forward, and bring the future of industry into the present. SMMs need a broader array of access options, training, support, and guidance. Providing access will supercharge any organization with tomorrow’s tools, as positively disruptive and potential-laden as the assembly line once was. Sustainable success in the State of Michigan requires the development of foundational infrastructure, the exploration of initial inroads with various manufacturers of all sizes, and the initiation of a prototype engagement mechanism applicable for other future regional efforts. To accomplish this NCMS leveraged complimen-tary State and Federal funding opportunities (shown in Figure 1) along with a coupled voice of industry market research study. A brief summary of each opportunity is found in Appendix A. At the heart of the Michigan effort was the development of an access portal (www.doitindigital.com) and the development of partnerships with local large manufacturers (OEMs) who could provide pull to encourage SMMs (current and future suppliers) to participate. Central to this entire effort was the opportunity that this Final Report documents corresponding to the specific tasks associated with the U.S. Department of Energy (DOE) funded component of the InnoState Jobs Innovation Accelerator Challenge (JIAC) Program.« less

ZMOTTO- MODELING THE INTERNAL COMBUSTION ENGINE

NASA Technical Reports Server (NTRS)

Zeleznik, F. J.

1994-01-01

The ZMOTTO program was developed to model mathematically a spark-ignited internal combustion engine. ZMOTTO is a large, general purpose program whose calculations can be established at five levels of sophistication. These five models range from an ideal cycle requiring only thermodynamic properties, to a very complex representation demanding full combustion kinetics, transport properties, and poppet valve flow characteristics. ZMOTTO is a flexible and computationally economical program based on a system of ordinary differential equations for cylinder-averaged properties. The calculations assume that heat transfer is expressed in terms of a heat transfer coefficient and that the cylinder average of kinetic plus potential energies remains constant. During combustion, the pressures of burned and unburned gases are assumed equal and their heat transfer areas are assumed proportional to their respective mass fractions. Even the simplest ZMOTTO model provides for residual gas effects, spark advance, exhaust gas recirculation, supercharging, and throttling. In the more complex models, 1) finite rate chemistry replaces equilibrium chemistry in descriptions of both the flame and the burned gases, 2) poppet valve formulas represent fluid flow instead of a zero pressure drop flow, and 3) flame propagation is modeled by mass burning equations instead of as an instantaneous process. Input to ZMOTTO is determined by the model chosen. Thermodynamic data is required for all models. Transport properties and chemical kinetics data are required only as the model complexity grows. Other input includes engine geometry, working fluid composition, operating characteristics, and intake/exhaust data. ZMOTTO accommodates a broad spectrum of reactants. The program will calculate many Otto cycle performance parameters for a number of consecutive cycles (a cycle being an interval of 720 crankangle degrees). A typical case will have a number of initial ideal cycles and progress through levels of nonideal cycles. ZMOTTO has restart capabilities and permits multicycle calculations with parameters varying from cycle to cycle. ZMOTTO is written in FORTRAN IV (IBM Level H) but has also been compiled with IBM VSFORTRAN (1977 standard). It was developed on an IBM 3033 under the TSS operating system and has also been implemented under MVS. Approximately 412K of 8 bit bytes of central memory are required in a nonpaging environment. ZMOTTO was developed in 1985.

Polygenetic Karsted Hardground Omission Surfaces in Lower Silurian Neritic Limestones: a Signature of Early Paleozoic Calcite Seas

NASA Astrophysics Data System (ADS)

James, Noel P.; Desrochers, André; Kyser, Kurt T.

2015-04-01

Exquisitely preserved and well-exposed rocky paleoshoreline omission surfaces in Lower Silurian Chicotte Formation limestones on Anticosti Island, Quebec, are interpreted to be the product of combined marine and meteoric diagenesis. The different omission features include; 1) planar erosional bedding tops, 2) scalloped erosional surfaces, 3) knobs, ridges, and swales at bedding contacts, and 4) paleoscarps. An interpretation is proposed that relates specific omission surface styles to different diagenetic-depositional processes that took place in separate terrestrial-peritidal-shallow neritic zones. Such processes were linked to fluctuations in relative sea level with specific zones of diagenesis such as; 1) karst corrosion, 2) peritidal erosion, 3) subtidal seawater flushing and cementation, and 4) shallow subtidal deposition. Most surfaces are interpreted to have been the result of initial extensive shallow-water synsedimentary lithification that were, as sea level fell, altered by exposure and subaerial corrosion, only to be buried by sediments as sea level rose again. This succession was repeated several times resulting in a suite of recurring polyphase omission surfaces through many meters of stratigraphic section. Synsedimentary cloudy marine cements are well preserved and are thus interpreted to have been calcitic originally. Aragonite components are rare and thought to have to have been dissolved just below the Silurian seafloor. Large molluscs that survived such seafloor removal were nonetheless leached and the resultant megamoulds were filled with synsedimentary calcite cement. These Silurian inner neritic-strandline omission surfaces are temporally unique. They are part of a suite of marine omission surfaces that are mostly found in early Paleozoic neritic carbonate sedimentary rocks. These karsted hardgrounds formed during a calcite-sea time of elevated marine carbonate saturation and extensive marine cement precipitation. The contemporaneous greenhouse atmosphere was supercharged with CO2 leading to profound surface karst under strongly acid rain. Younger peritidal omission surfaces, although potentially formed during aragonite or calcite sea times, would have been subject to very different terrestrial diagenetic process with lower atmospheric pCO2 values but increasingly complex biogenic soils producing dissimilar alteration features.

The continuous spin representations of the Poincare and super-Poincare groups and their construction by the Inonu-Wigner group contraction

NASA Astrophysics Data System (ADS)

Khan, Abu M. A. S.

We study the continuous spin representation (CSR) of the Poincare group in arbitrary dimensions. In d dimensions, the CSRs are characterized by the length of the light-cone vector and the Dynkin labels of the SO(d-3) short little group which leaves the light-cone vector invariant. In addition to these, a solid angle Od-3 which specifies the direction of the light-cone vector is also required to label the states. We also find supersymmetric generalizations of the CSRs. In four dimensions, the supermultiplet contains one bosonic and one fermionic CSRs which transform into each other under the action of the supercharges. In a five dimensional case, the supermultiplet contains two bosonic and two fermionic CSRs which is like N = 2 supersymmetry in four dimensions. When constructed using Grassmann parameters, the light-cone vector becomes nilpotent. This makes the representation finite dimensional, but at the expense of introducing central charges even though the representation is massless. This leads to zero or negative norm states. The nilpotent constructions are valid only for even dimensions. We also show how the CSRs in four dimensions can be obtained from five dimensions by the combinations of Kaluza-Klein (KK) dimensional reduction and the Inonu-Wigner group contraction. The group contraction is a singular transformation. We show that the group contraction is equivalent to imposing periodic boundary condition along one direction and taking a double singular limit. In this form the contraction parameter is interpreted as the inverse KK radius. We apply this technique to both five dimensional regular massless and massive representations. For the regular massless case, we find that the contraction gives the CSR in four dimensions under a double singular limit and the representation wavefunction is the Bessel function. For the massive case, we use Majorana's infinite component theory as a model for the SO(4) little group. In this case, a triple singular limit is required to yield any CSR in four dimensions. The representation wavefunction is the Bessel function, as expected, but the scale factor is not the length of the light-cone vector. The amplitude and the scale factor are implicit functions of the parameter y which is a ratio of the internal and external coordinates. We also state under what conditions our solutions become identical to Wigner's solution.

Vitamins and endurance training. Food for running or faddish claims?

PubMed

van der Beek, E J

1985-01-01

The inter-relationship of food and physical performance, food is considered as a conglomerate of nutrients and man is depicted as a kind of organic pudding. This 'machine' concept of human performance in combination with the mysticism surrounding vitamins, has led to the faddish belief that additional vitamins are necessary to improve physical performance by means of supercharging the metabolic processes in the body. Various vitamins and their dietary recommendations as well as the indicators for vitamin status are discussed. It is concluded that a marginal or subclinical deficiency state can be defined as an intermediate between optimal vitamin status and frank clinical deficiency. Marginal deficiency is characterised by biochemical values deviating from statistically derived reference limits as well as the absence of clinical signs and symptoms of vitamin deficiency. Besides the static, mostly biochemical, indicators of vitamin status, more functional indicators are considered, among them work capacity. An extensive historical review on depletion studies, epidemiological surveys and supplementation studies is presented. It is concluded that a restricted intake of some B-complex vitamins-individually and in combination-of approximately less than 35 to 45% of the recommended dietary allowance may lead to decreased endurance capacity within a few weeks. Studies on ascorbic acid (vitamin C) depletion and fat-soluble vitamin A deficiency have noted no decrease of endurance capacity. However, in a few recent epidemiological surveys, biochemical vitamin C deficiency was actually shown to decrease aerobic power. Although the general conclusion is that a reduced water-soluble vitamin intake decreases endurance capacity, it is believed that further controlled experimentation is needed with B-complex vitamins and vitamin C individually. Furthermore, usually employed reference limits for vitamins need reappraisal translating them into impairment limits. With respect to the available evidence, it can be concluded that supplementation of diet with either single or multivitamin preparations containing B-complex vitamins, vitamin C or E does not improve physical performance in athletes with a normal biochemical vitamin balance resulting from a well-balanced diet. Although vitamin supplementation does not seem to produce any effect when the diet is adequate, it is possible that vitamin B-complex supplementation is useful in sports with a high energy expenditure, because of the unavoidable consumption of 'empty calories' i.e. food products with a low nutrient density. The side effects of megavitamin supplementation are discussed briefly.

Tanker Argus: Re-supply for a LEO Cryogenic Propellant Depot

NASA Astrophysics Data System (ADS)

St. Germain, B.; Olds, J.; Kokan, T.; Marcus, L.; Miller, J.

The Argus reusable launch vehicle (RLV) concept is a single-stage-to-orbit conical, winged bodied vehicle powered by two liquid hydrogen/liquid oxygen supercharged ejector ramjets. The 3rd generation Argus launch vehicle utilizes advanced vehicle technologies along with a Maglev launch assist track. A tanker version of the Argus RLV is envisioned to provide an economical means of providing liquid fuel and oxidizer to an orbiting low-Earth orbit (LEO) propellant depot. This depot could then provide propellant to various spacecraft, including reusable orbital transfer vehicles used to ferry space solar power satellites to geo-stationary orbit. Two different tanker Argus configurations were analyzed. The first simply places additional propellant tanks inside the payload bay of an existing Argus reusable launch vehicle. The second concept is a modified Argus RLV in which the payload bay is removed and the vehicle propellant tanks are stretched to hold extra propellant. An iterative conceptual design process was used to design both Argus vehicles. This process involves various disciplines including aerodynamics, trajectory analysis, weights &structures, propulsion, operations, safety, and cost/economics. The payload bay version of tanker Argus, which has a gross mass of 256.3MT, is designed to deliver a 9.07MT payload to LEO. This payload includes propellant and the tank structure required to secure this propellant in the payload bay. The modified, pure tanker version of Argus has a gross mass of 218.6MT and is sized to deliver a full 9.07MT of propellant to LEO. The economic analysis performed for this study involved the calculation of many factors including the design/development and recurring costs of each vehicle. These results were used along with other economic assumptions to determine the "per kilogram" cost of delivering propellant to orbit. The results show that for a given flight rate the "per kilogram" cost is cheaper for the pure tanker version of Argus. However, the main goal of this study was to determine at which flight rate would it be financially beneficial to spend more development money to modify an existing, sunk cost, payload bay version of Argus in order to create a more efficient pure tanker version. For flight rates greater than approximately 320 flights/year, there is only a small financial motivation to develop a pure tanker version. At this flight rate both versions of Argus are able to deliver propellant to LEO at an approximate cost of 375/kg.

Synthetic genome engineering forging new frontiers for wine yeast.

PubMed

Pretorius, Isak S

2017-02-01

Over the past 15 years, the seismic shifts caused by the convergence of biomolecular, chemical, physical, mathematical, and computational sciences alongside cutting-edge developments in information technology and engineering have erupted into a new field of scientific endeavor dubbed Synthetic Biology. Recent rapid advances in high-throughput DNA sequencing and DNA synthesis techniques are enabling the design and construction of new biological parts (genes), devices (gene networks) and modules (biosynthetic pathways), and the redesign of biological systems (cells and organisms) for useful purposes. In 2014, the budding yeast Saccharomyces cerevisiae became the first eukaryotic cell to be equipped with a fully functional synthetic chromosome. This was achieved following the synthesis of the first viral (poliovirus in 2002 and bacteriophage Phi-X174 in 2003) and bacterial (Mycoplasma genitalium in 2008 and Mycoplasma mycoides in 2010) genomes, and less than two decades after revealing the full genome sequence of a laboratory (S288c in 1996) and wine (AWRI1631 in 2008) yeast strain. A large international project - the Synthetic Yeast Genome (Sc2.0) Project - is now underway to synthesize all 16 chromosomes (∼12 Mb carrying ∼6000 genes) of the sequenced S288c laboratory strain by 2018. If successful, S. cerevisiae will become the first eukaryote to cross the horizon of in silico design of complex cells through de novo synthesis, reshuffling, and editing of genomes. In the meantime, yeasts are being used as cell factories for the semi-synthetic production of high-value compounds, such as the potent antimalarial artemisinin, and food ingredients, such as resveratrol, vanillin, stevia, nootkatone, and saffron. As a continuum of previously genetically engineered industrially important yeast strains, precision genome engineering is bound to also impact the study and development of wine yeast strains supercharged with synthetic DNA. The first taste of what the future holds is the de novo production of the raspberry ketone aroma compound, 4-[4-hydroxyphenyl]butan-2-one, in a wine yeast strain (AWRI1631), which was recently achieved via metabolic pathway engineering and synthetic enzyme fusion. A peek over the horizon is revealing that the future of "Wine Yeast 2.0" is already here. Therefore, this article seeks to help prepare the wine industry - an industry rich in history and tradition on the one hand, and innovation on the other - for the inevitable intersection of the ancient art practiced by winemakers and the inventive science of pioneering "synthetic genomicists". It would be prudent to proactively engage all stakeholders - researchers, industry practitioners, policymakers, regulators, commentators, and consumers - in a meaningful dialog about the potential challenges and opportunities emanating from Synthetic Biology. To capitalize on the new vistas of synthetic yeast genomics, this paper presents wine yeast research in a fresh context, raises important questions and proposes new directions.

Dualities and Curved Space Partition Functions of Supersymmetric Theories

NASA Astrophysics Data System (ADS)

Agarwal, Prarit

In this dissertation we discuss some conjectured dualities in supersymmetric field theories and provide non-trivial checks for these conjectures. A quick review of supersymmetry and related topics is provided in chapter 1. In chapter 2, we develop a method to identify the so called BPS states in the Hilbert space of a supersymmetric field theory (that preserves at least two real supercharges) on a generic curved space. As an application we obtain the superconformal index (SCI) of 4d theories. The large N SCI of quiver gauge theories has been previously noticed to factorize over the set of extremal BPS mesonic operators. In chapter 3, we reformulate this factorization in terms of the zigzag paths in the dimer model associated to the quiver and extend the factorization theorem of the index to include theories obtained from D-branes probing orbifold singularities. In chapter 4, we consider the dualities in two classes of 3 dimensional theories. The first class consist of dualities of certain necklace type Chern-Simons (CS) quiver gauge theories. A non trivial check of these dualities is provided by matching their squashed sphere partition functions. The second class consists of theories whose duals are described by a collection of free fields. In such cases, due to mixing between the superconformal R-symmetry and accidental symmetries, the matching of electric and magnetic partition functions is not straightforward. We provide a prescription to rectify this mismatch. In chapter 5, we consider some the N = 1 4d theories with orthogonal and symplectic gauge groups, arising from N = 1 preserving reduction of 6d theories on a Riemann surface. This construction allows us to dual descriptions of 4d theories. Some of the dual frames have no known Lagrangian description. We check the dualities by computing the anomaly coefficients and the superconformal indices. We also give a prescription to write the index of the theory obtained by reduction of 6d theories on a three punctured sphere with Z2 and Z3 twist lines and verify that it exhibits the conjectured symmetry enhancement from G2 x U Sp(6) to E 7. In chapter 6, we continue our study of 4d theories obtained from reduction of 6d theories. We introduce a new type of object that we call the 'Fan' and show how to construct new N = 1 superconformal theories using the Fan. In chapter 7, we demonstrate the existence of an infinite number of theories that are either dual to or exhibit a cascade of RG flows down to the SU(N) SQCD with four flavors and a quartic superpotential.

Bioinspired Materials for Controlling Ice Nucleation, Growth, and Recrystallization.

PubMed

He, Zhiyuan; Liu, Kai; Wang, Jianjun

2018-05-15

Ice formation, mainly consisting of ice nucleation, ice growth, and ice recrystallization, is ubiquitous and crucial in wide-ranging fields from cryobiology to atmospheric physics. Despite active research for more than a century, the mechanism of ice formation is still far from satisfactory. Meanwhile, nature has unique ways of controlling ice formation and can provide resourceful avenues to unravel the mechanism of ice formation. For instance, antifreeze proteins (AFPs) protect living organisms from freezing damage via controlling ice formation, for example, tuning ice nucleation, shaping ice crystals, and inhibiting ice growth and recrystallization. In addition, AFP mimics can have applications in cryopreservation of cells, tissues, and organs, food storage, and anti-icing materials. Therefore, continuous efforts have been made to understand the mechanism of AFPs and design AFP inspired materials. In this Account, we first review our recent research progress in understanding the mechanism of AFPs in controlling ice formation. A Janus effect of AFPs on ice nucleation was discovered, which was achieved via selectively tethering the ice-binding face (IBF) or the non-ice-binding face (NIBF) of AFPs to solid surfaces and investigating specifically the effect of the other face on ice nucleation. Through molecular dynamics (MD) simulation analysis, we observed ordered hexagonal ice-like water structure atop the IBF and disordered water structure atop the NIBF. Therefore, we conclude that the interfacial water plays a critical role in controlling ice formation. Next, we discuss the design and fabrication of AFP mimics with capabilities in tuning ice nucleation and controlling ice shape and growth, as well as inhibiting ice recrystallization. For example, we tuned ice nucleation via modifying solid surfaces with supercharged unfolded polypeptides (SUPs) and polyelectrolyte brushes (PBs) with different counterions. We found graphene oxide (GO) and oxidized quasi-carbon nitride quantum dots (OQCNs) had profound effects in controlling ice shape and inhibiting ice growth. We also studied the ion-specific effect on ice recrystallization inhibition (IRI) with a large variety of anions and cations. All functionalities are achieved by tuning the properties of interfacial water on these materials, which reinforces the importance of the interfacial water in controlling ice formation. Finally, we review the development of novel application-oriented materials emerging from our enhanced understanding of ice formation, for example, ultralow ice adhesion coatings with aqueous lubricating layer, cryopreservation of cells by inhibiting ice recrystallization, and two-dimensional (2D) and three-dimensional (3D) porous materials with tunable pore sizes through recrystallized ice crystal templates. This Account sheds new light on the molecular mechanism of ice formation and will inspire the design of unprecedented functional materials based on controlled ice formation.

Integration of a wave rotor to an ultra-micro gas turbine (UmuGT)

NASA Astrophysics Data System (ADS)

Iancu, Florin

2005-12-01

Wave rotor technology has shown a significant potential for performance improvement of thermodynamic cycles. The wave rotor is an unsteady flow machine that utilizes shock waves to transfer energy from a high energy fluid to a low energy fluid, increasing both the temperature and the pressure of the low energy fluid. Used initially as a high pressure stage for a gas turbine locomotive engine, the wave rotor was commercialized only as a supercharging device for internal combustion engines, but recently there is a stronger research effort on implementing wave rotors as topping units or pressure gain combustors for gas turbines. At the same time, Ultra Micro Gas Turbines (UmuGT) are expected to be a next generation of power source for applications from propulsion to power generation, from aerospace industry to electronic industry. Starting in 1995, with the MIT "Micro Gas Turbine" project, the mechanical engineering research world has explored more and more the idea of "Power MEMS". Microfabricated turbomachinery like turbines, compressors, pumps, but also electric generators, heat exchangers, internal combustion engines and rocket engines have been on the focus list of researchers for the past 10 years. The reason is simple: the output power is proportional to the mass flow rate of the working fluid through the engine, or the cross-sectional area while the mass or volume of the engine is proportional to the cube of the characteristic length, thus the power density tends to increase at small scales (Power/Mass=L -1). This is the so-called "cube square law". This work investigates the possibilities of incorporating a wave rotor to an UmuGT and discusses the advantages of wave rotor as topping units for gas turbines, especially at microscale. Based on documented wave rotor efficiencies at larger scale and subsidized by both, a gasdynamic model that includes wall friction, and a CFD model, the wave rotor compression efficiency at microfabrication scale could be estimated at about 70%, which is much higher than the obtained efficiency obtained for centrifugal compressors in a microfabricated gas turbine. This dissertation also proposes several designs of ultra-micro wave rotors, including the novel concept of a radial-flow configuration. It describes a new and simplified design procedure as well as numerical simulations of these wave rotors. Results are obtained using FLUENT, a Computational Fluid Dynamics (CFD) commercial code. The vast information about the unsteady processes occurring during simulation is visualized. Last, two designs for experimental tests have been created, one for a micro shock tube and one for the ultra-micro wave rotor. Theoretical and numerical results encourage the idea that at microscale, compression by shock waves may be more efficient than by conventional centrifugal compressors, thus making the ultra-micro wave rotor (UmuWR) a feasible idea for enhancing (upgrading) UmuGT.

Effect of self recirculation casing treatment on the performance of a turbocharger centrifugal compressor

NASA Astrophysics Data System (ADS)

Gancedo, Matthieu

Increase in emission regulations in the transport industry brings the need to have more efficient engines. A path followed by the automobile industry is to downsize the size of the internal combustion engine and increase the air density at the intake to keep the engine power when needed. Typically a centrifugal compressor is used to force the air into the engine, it can be powered from the engine shaft (superchargers) or extracting energy contained into the hot exhaust gases with a turbine (turbochargers). The flow range of the compressor needs to match the one of the engine. However compressors mass flow operating range is limited by choke on the high end and surge on the low end. In order to extend the operation at low mass flow rates, the use of passive devices for turbocharger centrifugal compressors was explored since the late 80's. Hence, casing treatments including flow recirculation from the inducer part of the compressor have been shown to move the surge limit to lower flows. Yet, the working mechanisms are still not well understood and thus, to optimize the design of this by-pass system, it is necessary to determine the nature of the changes induced by the device both on the dynamic stability of the pressure delivery and on the flow at the inlet. The compressor studied here features a self-recirculating casing treatment at the inlet. The recirculation passage could be blocked to carry a direct comparison between the cases with and without the flow feature. To grasp the effect on compressor stability, pressure measurements were taken in the different constituting elements of the compressor. The study of the mean pressure variations across the operating map showed that the tongue region is a limiting element. Dynamic pressure measurements revealed that the instabilities generated near the inducer when the recirculation is blocked increase the overall instability levels at the compressor outlet and propagating pressure waves starting at the tongue occurred, different in nature from rotating stall. The flow velocity was also measured at the inlet of the compressor by means of planar PIV measurements. The case without recirculation showed strong back flow occurrence at low MFR on the shroud of the inlet passage due to tip recirculation. With recirculation, this back flow was significantly reduced improving the overall stability. However, with the current recirculation channels design, there is an efficiency penalty and the recirculated flow introduces non-homogeneities in the mixing region. Finally, to explore experimentally the effect of variations of the casing treatment, several different designs were tested. It was seen that modifications of the supporting rib shape impacted the efficiency. Also, improvements on the surge line were obtained with flow reinjection near the inducer in the direction of the main flow at low speeds and with induced counter swirl for all speeds.

Detroit Commuter Hydrogen Project

DOE Office of Scientific and Technical Information (OSTI.GOV)

Brooks, Jerry; Prebo, Brendan

2010-07-31

This project was undertaken to demonstrate the viability of using hydrogen as a fuel in an internal combustion engine vehicle for use as a part of a mass transit system. The advantages of hydrogen as a fuel include renew-ability, minimal environmental impact on air quality and the environment, and potential to reduce dependence on foreign energy sources for the transportation sector. Recognizing the potential for the hydrogen fuel concept, the Southeast Michigan Congress of Governments (SEMCOG) determined to consider it in the study of a proposed regional mass transit rail system for southeast Michigan. SEMCOG wanted to evaluate the feasibilitymore » of using hydrogen fueled internal combustion engine (H2ICE) vehicles in shuttle buses to connect the Detroit Metro Airport to a proposed, nearby rail station. Shuttle buses are in current use on the airport for passenger parking and inter-terminal transport. This duty cycle is well suited to the application of hydrogen fuel at this time because of the ability to re-fuel vehicles at a single nearby facility, overcoming the challenge of restricted fuel availability in the undeveloped hydrogen fuel infrastructure. A cooperative agreement between SEMCOG and the DOE was initiated and two H2ICE buses were placed in regular passenger service on March 29, 2009 and operated for six months in regular passenger service. The buses were developed and built by the Ford Motor Company. Wayne County Airport Authority provided the location for the demonstration with the airport transportation contractor, Metro Cars Inc. operating the buses. The buses were built on Ford E450 chassis and incorporated a modified a 6.8L V-10 engine with specially designed supercharger, fuel rails and injectors among other sophisticated control systems. Up to 30 kg of on-board gaseous hydrogen were stored in a modular six tank, 350 bar (5000 psi) system to provide a 150 mile driving range. The bus chassis and body were configured to carry nine passengers with luggage. By collecting fuel use data for the two H2ICE buses, with both written driver logs and onboard telemetry devices, and for two conventional propane-gasoline powered buses in the same service, comparisons of operating efficiency and maintenance requirements were completed. Public opinion about the concept of hydrogen fuel was sampled with a rider survey throughout the demonstration. The demonstration was very effective in adding to the understanding of the application of hydrogen as a transportation fuel. The two 9 passenger H2ICE buses accumulated nearly 50,000 miles and carried 14,285 passengers. Data indicated the H2ICE bus fuel economy to be 9.4 miles/ gallon of gasoline equivalent (m/GGE) compared to the 10 passenger propane-gasoline bus average of 9.8 m/GGE over 32,400 miles. The 23- passenger bus averaged 7.4 m/GGE over 40,700 miles. Rider feedback from 1050 on-board survey cards was overwhelmingly positive with 99.6% indicating they would ride again on a hydrogen powered vehicle. Minimal maintenance was required for theses buses during the demonstration project, but a longer duration demonstration would be required to more adequately assess this aspect of the concept.« less

Precursory swarms of long-period events at Redoubt Volcano (1989-1990), Alaska: Their origin and use as a forecasting tool

USGS Publications Warehouse

Chouet, B.A.; Page, R.A.; Stephens, C.D.; Lahr, J.C.; Power, J.A.

1994-01-01

During the eruption of Redoubt Volcano from December 1989 through April 1990, the Alaska Volcano Observatory issued advance warnings of several tephra eruptions based on changes in seismic activity related to the occurrence of precursory swarms of long-period (LP) seismic events (dominant period of about 0.5 s). The initial eruption on December 14 occurred after 23 years of quiescence and was heralded by a 23-hour swarm of LP events that ended abruptly with the eruption. After a series of vent-clearing explosions over the next few days, dome growth began on December 21. Another swarm, with LP events similar to those of the first, began on the 26th and ended in a major tephra eruption on January 2. Eruptions continued over the next two weeks and then ceased until February 15, when a large eruption initiated a long phase of repetitive dome-building and dome-destroying episodes that continued into April. Warnings were issued before the major events on December 14 and January 2, but as the eruptive sequence continued after January 2, the energy of the swarms decreased and forecasting became more difficult. A significant but less intense swarm preceded the February 15 eruption, which was not forecast. This eruption destroyed the only seismograph on the volcanic edifice and stymied forecasting until March 4, when the first of three new stations was installed within 3 km of the active vent. From March 4 to the end of the sequence on April 21, there were eight eruptions, six of which were preceded by detectable swarms of LP events. Although weak, these swarms provided the basis for warnings issued before the eruptions on March 23 and April 6. The initial swarm on December 13 had the following features: (1) short duration (23 hours); (2) a rapidly accelerating rate of seismic energy release over the first 18 hours of the swarm, followed by a decline of activity during the 5 hours preceding the eruption; (3) a magnitude range from -0.4 to 1.6; (4) nearly identical LP signatures with a dominant period near 0.5 s; (5) dilatational first motions everywhere; and (6) a stationary source location at a depth of 1.4 km beneath the crater. This occurrence of long-period events suggests a model involving the interaction of magma with groundwater in which magmatic gases, steam and water drive a fixed conduit at a stationary point throughout the swarm. The initiation of that sequence of events is analogous to the failure of a pressure-relief valve connecting a lower, supercharged magma-dominated reservoir to a shallow hydrothermal system. A three-dimensional model of a vibrating fluid-filled crack recently developed by Chouet is found to be compatible with the seismic data and yields the following parameters for the LP source: crack length, 280-380 m; crack width, 140-190 m; crack thickness, 0.05-0.20 m; crack stiffness, 100-200; sound speed of fluid, 0.8-1.3 km/s; compressional-wave speed of rock, 5.1 km/s; density ratio of fluid to rock, ???0.4; and ratio of bulk modulus of fluid to rigidity of rock, 0.03-0.07. The fluid-filled crack is excited intermittently by an impulsive pressure drop that varies in magnitude within the range of 0.4 to 40 bar. Such disturbance appears to be consistent with a triggering mechanism associated with choked flow conditions in the crack. ?? 1994.

Electron Transport in SrTio3 Accumulation Layers and Semiconductor Nanocrystal Films

NASA Astrophysics Data System (ADS)

Fu, Han

In this thesis, we study two subjects: SrTiO3 (STO) accumulation layers and films made of semiconductor nanocrystals (NCs), which are important for technological applications. We start from the low temperature conductivity of electron accumulation layers induced by the very strong electric field at the surface of STO sample. Due to the strongly nonlinear lattice dielectric response, the three-dimensional density of electrons n(z) in such a layer decays with the distance from the surface z very slowly as n(z) ≃ 1/z12/7 . We show that when the mobility is limited by the surface scattering the contribution of such a tail to the conductivity diverges at large z because of growing time electrons need to reach the surface. We explore truncation of this divergence by the finite sample width, by the bulk scattering rate, by the back gate voltage, or by the crossover to the bulk linear dielectric response with the dielectric constant kappa. As a result we arrive at the anomalously large mobility, which depends not only on the rate of the surface scattering, but also on the physics of truncation. Similar anomalous behavior is found for the Hall factor, the magnetoresistance, and the thermopower. For the second part, we extend to the cases of spherical and cylindrical geometries, and more complicated planar structures. For the planar case, we study overlapping accumulation layers in GdTiO3/STO/GdTiO 3 quantum wells and electron gases created by spill-out from NSTO (heavily n-type doped STO) layers into STO. Generalization of our approach to a spherical donor cluster creating a big Thomas-Fermi atom with electrons in STO brings us to the problem of supercharged nuclei. It is known that for an atom with nuclear charge Ze, where Z > 170, electrons collapse onto the nucleus resulting in a net charge Zn < Z. Here, instead of relativistic physics, the collapse is caused by the nonlinear dielectric response. Electrons collapse into the charged spherical donor cluster with radius R when its total charge number Z exceeds the critical value Zc ≃ R/a, where a is the lattice constant. The net charge eZ n grows with Z until Z exceeds Z*≃ (R/a)9/7. After this point, the charge number of the compact core Zn remains ≃ Z*, with the rest Z electrons forming a sparse Thomas-Fermi atom with it. We also study the case of long cylindrical clusters. In the third part, we look at the details of the surface scattering by roughness of accumulation layers. To connect with previous works on surface roughness scattering, we focus on conventional semiconductors with the linear dielectric response where accumulation layers with very large concentrations of electrons and many subbands filled became recently available due to ionic liquid and other new methods of gating. The low temperature mobility in such layers is limited by the surface roughness scattering. However theories of roughness scattering so far dealt only with the small-density single subband two-dimensional (2D) electron gas. Here we develop a theory of roughness scattering limited mobility for the multisubband large concentration case. We show that with growing 2D electron concentration N the surface dimensionless conductivity sigma/(2e2/h) first decreases as ≃ N-6/5 and then saturates as ˜ (LambdaaB/Delta 2) >> 1, where Lambda and Delta are the characteristic length and height of the surface roughness, aB is the effective Bohr radius. This means that in spite of the shrinkage of the 2D electron gas width and the related increase of the scattering rate, the 2D electron gas remains a good metal. Thus, there is no re-entrant metal-insulator transition at high concentrations conjectured by Das Sarma and Hwang [PRB 89, 121413 (2014)]. The expression of surface relaxation time can be generalized to the STO case where the dielectric response is nonlinear. We find that there is no reentrant metal-insulator transition, either, in STO accumulation layers at experimentally available large N.. Finally, we switch to the study of NC films. We focus on the variable-range hopping of electrons in semiconductor NC films below the critical doping concentration nc at which films become metallic. The hopping conductivity is then described by the Efros-Shklovskii law which depends on the localization length of electrons. We study how the localization length grows with the doping concentration n in the film of touching NCs. For that we calculate the electron transfer matrix element t(n) between neighboring NCs for two models when NCs touch by small facets or just one point. We study two sources of disorder: variations of NC diameters and random Coulomb potentials originating from random numbers of donors in NCs. We use the ratio of t(n) to the disorder-induced NC level dispersion to find the localization length of electrons due to the multi-step elastic co-tunneling process. We find three different phases at n < nc depending on the strength of disorder, the material, sizes of NCs and their facets: 1) "insulator" where the localization length of electrons increases monotonically with n and 2) "oscillating insulator" when the localization length (and the conductivity) oscillates with n from the insulator base and 3) "blinking metal" where the localization length periodically diverges. The first two phases were seen experimentally and we discuss how one can see the more exotic third one. In all three the localization length diverges at n = nc. This allows us to find nc..

hwhap_Ep16_Spacesuits

NASA Image and Video Library

2017-10-26

>> HOUSTON, WE HAVE A PODCAST. WELCOME TO THE OFFICIAL PODCAST OF THE NASA JOHNSON SPACE CENTER, EPISODE 16: SPACESUITS. I’M GARY JORDAN AND I’LL BE YOUR HOST TODAY. SO IF YOU’RE NEW TO THE SHOW, THIS IS WHERE WE BRING IN NASA EXPERTS-- SCIENTISTS, ENGINEERS, ASTRONAUTS-- ALL TO TELL YOU THE COOLEST PARTS ABOUT WHAT’S GOING ON HERE AT NASA. SO ALLYOOP ON TWITTER IS ASKING IF WE CAN DO AN EPISODE ON SPACESUITS. WELL, THANKS FOR YOUR SUGGESTION, ALLYOOP. LET’S DO IT! TODAY WE’RE TALKING SPACESUITS WITH LES PADILLA. HE’S THE EMU HARDWARE MANAGER AT THE NASA JOHNSON SPACE CENTER IN HOUSTON, TEXAS, AND THAT JUST MEANS HE MANAGES THE HARDWARE ON THOSE CLASSIC WHITE SPACESUITS YOU SEE WHEN YOU THINK ABOUT ASTRONAUTS. WE HAD A GREAT DISCUSSION ABOUT HOW THOSE SPACESUITS WORK, WHAT THEY’RE MADE OF, HOW THEY’VE EVOLVED OVER TIME, AND WHAT THEY’LL LOOK LIKE IN THE FUTURE. SO WITH NO FURTHER DELAY, LET’S GO LIGHT SPEED AND JUMP RIGHT AHEAD TO OUR TALK WITH MR. LES PADILLA. ENJOY. [ MUSIC ] >> T MINUS FIVE SECONDS AND COUNTING-- MARK. [ INDISTINCT RADIO CHATTER ] >> HOUSTON, WE HAVE A PODCAST. [ MUSIC ] >> I LIKE TO EXPLAIN TO OTHERS, I FEEL LIKE A KID IN A CANDY STORE WHEN THEY ASK ABOUT IT. >> YEAH. >> IT’S AWESOME TO BOTH SEE THE PAST WHERE IT CAME FROM AND THE FUTURE DESIGNS WHERE WE’RE MAYBE HEADED TOWARDS. >> THAT’S RIGHT, AND THAT’S WHAT WE’RE GOING TO TALK ABOUT TODAY, ALL OF THOSE THINGS. >> ALL RIGHT. >> SO I HOPE YOU-- I SEE YOU HAVE A LARGE BINDER OF NOTES. IT’S ACTUALLY ONE PAGE. BUT YEAH, SO WE’RE GOING TO TALK ABOUT IT ALL TODAY. SO FIRST OF ALL, SPACESUITS. LET’S START FROM LIKE THE OVERARCHING, LIKE WHAT IS A SPACESUIT, WHY DO YOU NEED A SPACESUIT? I THINK THE CLOSEST THING THAT I’VE BEEN DESCRIBED IS LIKE THINK OF IT LIKE A SPACESHIP THAT’S SHAPED LIKE A HUMAN BODY. IS THAT KIND OF RIGHT? >> THAT’S A FANTASTIC DESCRIPTION RIGHT THERE. >> COOL. >> A LOT BETTER AND A LOT SHORTER THAN I COULD’VE SAID IT. >> OKAY SO WHAT ARE THEY, HOW, LIKE WHY A SPACESUIT? WHY DO WE NEED THAT? WHY CAN’T WE JUST USE THE FANCY SPACECRAFT WITH LIKE ARMS ON IT OR SOMETHING LIKE THAT? >> YEAH, SO AT SOME POINT, PEOPLE BEFORE US DECIDED, “WE WANT TO GO TO SPACE.” AND AFTER THAT THEY DECIDED GOING TO SPACE WASN’T ENOUGH. WE WANT TO GO EXTRAVEHICULAR, OUTSIDE THE SPACESHIP-- WHATEVER SPACESHIP IT IS, FROM SHUTTLE TO STATION, TO BEFORE THOSE AND THE MERCURY MISSIONS ALL THE WAY IN THE EARLY DAYS. AND THE SPACESUIT, THE PURPOSE OF IT IS TO BE SORT OF AS YOU SAID, A MINIATURE AIRCRAFT, BUT ALLOW US MOBILITY, FLEXIBILITY, MANEUVERABILITY, SO THAT A CREW MEMBER COULD MOVE AROUND WHEN THEY’RE DOING WORK OR JUST EXPERIENCING THE ENVIRONMENT OUT THERE. LIKE IN THE EARLY DAYS IN GEMINI WHEN THEY WENT OUT THE DOOR. >> THAT’S RIGHT, ED WHITE. >> YEAH, ABSOLUTELY, YOU GOT IT. JUST EXPERIENCING THE ENVIRONMENT, DID NOT WANT TO COME BACK IN. >> YEAH. >> OR LATER DAYS, EVEN WHERE WE ARE RIGHT NOW WITH THE INTERNATIONAL SPACE STATION, WHERE THERE ARE MAINTENANCE ACTIVITIES AND THERE IS-- WE’VE ALREADY COMPLETED THE ASSEMBLY, SO IT’S MAINTENANCE ACTIVITIES IS WHERE WE’RE AT. WE NEED TO BE ABLE TO GO OUT THERE AND DO MORE THAN JUST FLY AROUND AND ENJOY THE SCENERY. WE NEED TO BE ABLE TO TURN BOLTS. WE NEED TO BE ABLE TO PULL OUT LARGE BATTERIES AND PUT THEM BACK IN. AND SO THEY NEED SOMETHING THAT OFFERS DEXTERITY AND YET PROTECTION FROM THE VERY HARSH SPACE ENVIRONMENT. >> YOU KNOW, WE JUST SAW THAT, BECAUSE WE JUST DID THE SPACEWALK THE OTHER DAY, RIGHT. THAT WAS THE SECOND OF THREE PLANNED ONES, AND THAT WAS WHEN THEY WERE PUTTING ON SOME OF THE SHIELDS AND EVERYTHING. >> ABSOLUTELY. >> AND THEY DID SOME ROBOTIC WORK, RIGHT, WITH THE STATION’S ROBOTIC ARM. THEY TOOK THE PRESSURIZED MATING ADAPTOR, MOVED IT TO A NEW PLACE, BUT THEY NEEDED HUMAN HANDS TO ACTUALLY CONNECT THE CABLES AND ACTUALLY PUT ON THE SHIELDS. SO IT MAKES SENSE, RIGHT-- YOU NEED THE SUITS BECAUSE THERE’S SOME THINGS THAT ROBOTS JUST CAN’T DO, I GUESS, RIGHT? >> YEAH, NOT YET, NOT WHERE WE ARE TODAY. YOU CAN’T GO TO SPACE WITHOUT EVA. >> YEAH, THAT’S TRUE. OKAY, SO LIKE GOING BACK TO ED WHITE AND GEMINI, THAT WAS-- THE FIRST ONE WAS-- OH, NO, I HAD-- I JUST HAD IT. I WANT TO SAY JUNE 1965? ‘65, THERE IT IS. ALL RIGHT, YEAH. HE CAME OUT AND THEY ACTUALLY USED THE AIR GUN TO MOVE AROUND. AND SUPER FAMOUS VIDEO OF WATCHING HIM JUST LIKE DRIFT OUT, AND HE’S GOT THE UMBILICAL, AND HE’S GOT THE AIR. SO I’VE GOT TO ASK-- WHAT WAS THE POINT OF THAT AIR GUN THINGY? AND THEN WHY DO WE NOT SEE ANYONE USE THOSE ANYMORE? >> YEAH, GREAT QUESTION, YEAH. AND SO THERE’S PROBABLY PEOPLE WISER AND MORE EXPERIENCED THAT HAVE EXTRA DETAILS ON THAT, BUT AT A HIGH, GENERAL LEVEL IT’S JUST DIRECTIONAL CONTROL. SO YOU’RE OUT THERE IN SPACE. WE CALL IT-- WE SAY NO GRAVITY. THERE IS SOME GRAVITY, BUT IT’S MICROGRAVITY, VERY LOW, AND FOR ALL INTENTS AND PURPOSES YOU’RE FREEFALLING TOWARDS THE EARTH. AND SO UNLESS YOU’RE HOLDING ONTO A HANDRAIL OR THE VEHICLE ITSELF, YOU WILL CONTINUE TO FLOAT, AND THE GRAVITATIONAL PULL TO THE SURFACE OF EARTH WILL BEGIN TO BRING YOU DOWN. SO AS SOON AS YOU GO OUT THAT DOOR, YOU’VE GOT TO HAVE A WAY-- IT COULD BE A TETHER OR A ROPE TO PULL YOU BACK IN, BUT A WAY TO MANEUVER AROUND THE AREA YOU WANT TO GO. AND SO THE AIR GUN PROVIDES A SMALL PROPULSION CAPABILITY TO NAVIGATE. >> OKAY, MAKES A LOT OF SENSE. SO, OKAY, THEY’RE GOING OUT AND USING THE AIR GUN, BUT NOW I GUESS THEY HAVE-- IT TOOK THEM A WHILE, RIGHT, DURING THE GEMINI? THAT WAS KIND OF A LOT OF THE POINT OF THE GEMINI PROGRAM, WAS TO FIGURE OUT HOW TO DO STUFF LIKE THIS, HOW TO DO SPACE RENDEZVOUS, AND HOW TO DO SPACEWALKS. IT TOOK THEM A WHILE, RIGHT? SO THAT WAS GEMINI 4 WAS WHEN ED WHITE CAME OUT. AND THEN IT WASN’T UNTIL GEMINI 12, BUZZ ALDRIN HAD PUT IN SOME PROCEDURES FOR NEUTRAL BUOYANCY LABORATORY TRAINING, WHERE THEY ACTUALLY TRAIN IN THE WATER TO SEE HOW THEY CAN MOVE AROUND, BECAUSE EVERYONE WAS GETTING SORT OF TIRED WHEN THEY WERE GOING OUT BECAUSE THEY DIDN’T HAVE THE PROCEDURES YET. AND THEY FINALLY NAILED IT FOR GEMINI 12, RIGHT? >> YES. SPACEWALKS ARE TOUGH, TOUGH JOBS. >> YEAH. >> THE ASTRONAUTS ARE JUST AMAZING THE WAY THEY DO WORK SO SEAMLESSLY. AND AS TRAINED PROFESSIONALS, THEY MAKE IT SEEM EASY, BUT INSIDE THOSE SUITS-- BECAUSE I’VE SEEN THE SUITS COME OUT-- THERE’S A LOT OF SWEAT IN THERE. THERE’S A LOT OF HARD WORK THAT GOES ON FOR THOSE ASTRONAUTS, AND IT IS NOT EASY. AND AS YOU SAID, TRAINING ON THE GROUND IS PIVOTAL TO BE ABLE TO MAKE THOSE ACTIVITIES LOOK SEAMLESS ON ORBIT. >> YEAH, I’M TOTALLY NOT FOLLOWING THE SCRIPT RIGHT NOW, BUT I MEAN, SO THE NBL TRAINING THAT THEY DO, THEY DO IT IN THE NEUTRAL BUOYANCY LABORATORY-- SUPER BIG POOL. THEY HAVE LIKE 1-TO-1 SCALE MOCKUPS OF THE OUTSIDE OF THE INTERNATIONAL SPACE STATION, SO WHEN THEY ACTUALLY GO UP THERE AND THEY-- WELL, IN THE NEUTRAL BUOYANCY LABORATORY, THEY TRAIN IN A SPACESUIT, PRETTY MUCH. SO THEY KNOW EXACTLY HOW IT FEELS, AND WHERE THINGS ARE, AND THEY KNOW HOW TO MOVE FROM PLACE TO PLACE AND USE PROPER TOOLS. BECAUSE ONCE YOU’RE OUT THERE, YOU’VE GOT TO KNOW KIND OF WHAT YOU’RE DOING AND WHAT TO EXPECT, BECAUSE YOU MIGHT ENCOUNTER SOME HURDLES. AND THERE HAVE BEEN SOME HURDLES IN THE PAST. >> THERE HAVE BEEN, ABSOLUTELY. ALL IN THAT NEUTRAL BUOYANCY LAB, YOU’RE RIGHT. THEY ACTUALLY TRAIN IN A SPACESUIT THAT IS ALMOST EXACTLY LIKE THE ONES THEY FLY IN. SMALL LITTLE DIFFERENCES, LIKE THE WHITE BACKPACK, WHICH IS THE ENGINE OF THE SPACESUIT, THE PRIMARY LIFE SUPPORT SYSTEM. IN THE NEUTRAL BUOYANCY LAB, IT IS JUST A HOLLOW SHELL AND WE HAVE UMBILICALS, LONG HOSES, THAT SUPPLY THE AIR AND THE POWER TO THE SUIT. >> RIGHT. >> AND THE TOOLS WILL HAVE THINGS THAT ARE CHANGED ON THEM TO MAKE THEM MORE NEUTRAL BUOYANT, SO THEY’LL FLOAT IN WATER AND DON’T SINK DIRECTLY DOWN TO THE BOTTOM OF THE POOL. BUT OVERALL, IT IS, AS YOU POINTED OUT, JUST LIKE THE FLIGHT HARDWARE, AND THE SUITS ARE VERY SIMILAR TO WHAT THEY USE ON ORBIT SO THEY CAN TRAIN AND BE PREPARED. BECAUSE AS YOU NOTED, THERE IS NO GO OUT THE DOOR AND, “I’M NOT QUITE SURE WHAT I’M DOING OUT HERE. LET’S GO AHEAD AND PLAN ANOTHER DAY.” >> “LET’S FIGURE IT OUT. OH, WE CAN’T DO IT. I GUESS WE’LL COME OUT AGAIN.” BECAUSE YEAH, IT TAKES A LONG TIME, RIGHT? BECAUSE I MEAN, I WAS LISTENING TO SHANE THE OTHER DAY, BECAUSE HE JUST LANDED A COUPLE DAYS AGO AT THE TIME OF THIS RECORDING, AND HE WAS SAYING IT TAKES HOURS OF PREP WORK BEFOREHAND, RIGHT, LIKE FOUR HOURS. THEY’VE GOT TO PRE-BREATHE, THEY’VE GOT TO DO ALL THESE THINGS, PUT ON THE SUIT, AND THEN THEY GO OUT AND IT’S ANOTHER SEVEN-ISH HOURS THAT THEY’RE OUT THERE. THEN THEY COME BACK AND THEY HAVE LIKE A TWO-HOUR DEBRIEF. I MEAN, THAT’S A LONG DAY. HE CALLED IT ONE OF THE MOST CHALLENGING-- ESPECIALLY PHYSICALLY AND MENTALLY-- CHALLENGING THINGS ABOUT FLYING IN SPACE. >> YEAH. >> I CAN IMAGINE. AND ESPECIALLY-- I MEAN, THAT’S WHAT THEY TRAIN FOR, RIGHT? >> THAT’S RIGHT. >> IN THE NEUTRAL BUOYANCY LABORATORY THEY DO LIKE SIX-HOUR RUNS OR SOMETHING LIKE THAT. KIND OF THE SAME, THEY DO SOME PREP WORK BEFOREHAND. BUT THEY GET USED TO IT, AND THEY DO A LOT OF THAT TRAINING. >> SO I’VE NEVER BEEN, OBVIOUSLY, OUT THE DOOR IN SPACE. I’VE NEVER BEEN AN ASTRONAUT IN THAT ASPECT, BUT GARY, ONE OF THE BEST WAYS THAT I CAN DESCRIBE WHAT YOU JUST SAID IS HAVE YOU EVER GONE SKYDIVING? >> I HAVE, ONE TIME! >> YES, THEN YOU KNOW! SO THE STIMULI WHEN YOU MAKE THAT DECISION OF “ALL RIGHT, I’M ABOUT TO GET OUT OF A PERFECTLY GOOD AIRPLANE,” AND YOU GO OUT, JUST EVERYTHING GOING ON. IT IS-- THE FIRST TIME YOU GO, IT’S VERY HARD TO CONCENTRATE. >> OH, YEAH. >> IT’S KIND OF GOOD WITH THAT TANDEM THING, THE GUY GOING, “LOOK AT YOUR ALTIMETER.” [ LAUGHTER [ BUT IMAGINE FREEFALLING LIKE THAT FOR SEVEN HOURS STRAIGHT WHILE HAVING TO DO MAINTENANCE WORK ON THE SPACE STATION AND WATCH YOUR DISPLAY CONTROL MODULE ON YOUR EMU AND LISTEN TO PEOPLE ON THE GROUND AND INSIDE THE STATION. AND THAT’S JUST A SHADOW OF THE DIFFICULTY OF THE JOB THAT THOSE GUYS DO. >> OKAY, WELL, WHEN I WENT OUT THE DOOR FOR WHENEVER I WENT SKY DIVING, MY LEGS WENT WEAK AND I ALWAYS HAD THE GUY STRAPPED TO MY BACK, AND HE HAD TO LIKE PUSH FORWARD TO THE END OF THE DOOR AND ACTUALLY LIKE PUSH ME OUT. HE DID THE WHOLE LIKE INSTEAD OF “WE’RE GOING TO GO OUT ON THREE. ONE, TWO,” AND THEN WE WENT OUT. SO I WAS LIKE-- I WAS TOTALLY WEAK, BUT I CAN’T EVEN IMAGINE. BECAUSE MY HEART DROPPED ON THAT FIRST RUN, AND THEN IT WAS THRILLING FOR A WHILE. BUT I MEAN, EVERYTHING HAPPENED SO FAST. AND NOW LIKE YOU SAID, TAKE THAT AND THEN STRETCH IT OVER A SUPER LONG PERIOD. I CAN ONLY IMAGINE. OKAY, SO LET’S TAKE A STEP BACK AND LET’S GO BACK TO KIND OF WHERE I WAS ORIGINALLY SUPPOSED TO GO, BUT TALKING ABOUT SPACESUITS, AND FIRST OF ALL, WHY DO WE NEED IT? >> SURE. >> YOU KNOW, YOU NEED THE DEXTERITY, OBVIOUSLY, BUT THERE’S A HUMAN ASPECT TO THAT, RIGHT? YOU CAN’T JUST, “OH, YOU KNOW WHAT, SOMETHING’S BROKEN ON THE OUTSIDE. LET’S JUST GO OUT THE HATCH AND TORQUE IT--” TORQUE IT, WHAT AM I SAYING? “TORQUE IT WITH A WRENCH OR SOMETHING AND FIX IT.” YOU NEED, LIKE YOU SAID, YOU HINTED AT LIFE SUPPORT A WHILE BACK WITH THE BACKPACK. SO WHAT’S IT ABOUT-- THIS MAY SEEM A BIT OBVIOUS OF A QUESTION, BUT WHAT’S IT ABOUT SPACE THAT THE HUMAN BODY CANNOT JUST GO OUT AND DO TASKS IN? >> SURE, AND YOU KNOW, I THINK MOST PEOPLE COULD TELL YOU THAT SPACE, YEAH, IT’S A DANGEROUS ENVIRONMENT. BUT WHY IS IT IS WE’RE GETTING AT-- WELL, THE SPACESUIT PROVIDES THE CAPABILITY TO REGULATE TEMPERATURE. IN THE LOW EARTH ORBIT, AS WE CALL IT, WHERE THE INTERNATIONAL SPACE STATION IS, TEMPERATURE RANGES DURING THE EVA DAYS CAN SWING FROM NEGATIVE 148 DEGREES-- SO THAT’S 148 DEGREES FAHRENHEIT BELOW ZERO UP TO 248 DEGREES. AND THOSE ARE ESTIMATES THAT CAN BE HIGHER OR LOWER, BUT THAT’S A HUGE WINDOW THAT THE HUMAN ANATOMY WAS NOT DESIGNED TO WORK WITHIN WITHOUT PROTECTION. >> YEAH, I FEEL LIKE HOUSTON, TEXAS CAN GET UP TO ABOUT POSITIVE 248 DEGREES, BUT-- I KNOW IT’S NOT EVEN CLOSE, BUT-- >> NOT NEGATIVE 148, THOUGH. >> NO, NOT EVEN-- NO, NOT EVEN 148 TO ME. BUT YOU’RE RIGHT, THAT’S INTENSE. SO HOW DOES THE SPACESUIT PROTECT FROM THAT, THE EXTREME NEGATIVE AND POSITIVE TEMPERATURES? >> YEAH, SO THERE’S A LOT OF PLANNING UP FRONT IN CHOOSING DAYS THAT WE GO EVAs, WE CALL IT-- EXTRAVEHICULAR ACTIVITIES. >> THANK YOU. >> SPACEWALKS. >> WE TRY TO STAY AWAY FROM THOSE ACRONYMS, BUT YES, SPACEWALKS, RIGHT. >> WE CHOOSE SPECIAL DAYS THAT HAVE THE LEAST IMPACT-- MORE HABITABLE CONDITIONS WOULD BE A BETTER WAY TO PUT IT. BUT AT THE END OF THE DAY, EVEN ON THE BEST DAYS, TEMPERATURE SWINGS WHEN THE SUN’S LOOKING AT YOU TO WHEN THE SUN’S BEHIND THE STATION ARE LARGE SWINGS THAT CAN BE 100 DEGREES. AND SO THAT’S WHERE THE SPACESUIT COMES INTO PLAY. AND THE SPACESUIT WAS DESIGNED TO WORK IN THESE ENVIRONMENTS. THERE ARE-- THE OUTER LAYER IS WHITE BECAUSE IT REFLECTS HEAT. >> AH. >> LITTLE SIMPLE THINGS LIKE THAT. >> OKAY, NOW YOU KNOW WHY THE SPACESUITS ARE WHITE. >> THERE YOU GO. ALL RIGHT, WHEREAS IF IT WERE BLACK IT WOULD ABSORB THE HEAT, GET A LOT HOTTER QUICKER, AND MAKE IT HARD FOR THE PERFORMANCE OF THE SUIT AND THE INDIVIDUAL INSIDE. THE MULTIPLE INSULATION LAYERS ON THE SUIT ITSELF-- THERE ARE SEVEN LAYERS OF INSULATION WITHIN THE OUTER LAYER OF THE SPACESUIT. >> OH. >> AND WITHOUT GETTING INTO DETAILS, THOSE ARE SPECIFICALLY TO REFLECT HEAT AND TO PROTECT THE CREW MEMBERS, AND KEEP IN THE PROPER ENVIRONMENT HEAT THAT’S NECESSARY INSIDE THE SUIT. >> OKAY. >> SO IT MAY BE HOT OUT THERE, BUT WHEN THAT SUN GOES BEHIND STATION, IT GETS VERY COLD. THAT CREW MEMBER WANTS A CERTAIN AMOUNT OF HEAT KEPT WITHIN THAT SPACESUIT. >> I WOULD THINK SO, YEAH. >> ABSOLUTELY, ABSOLUTELY. >> NEGATIVE 148 IS PRETTY COLD. >> BUT LOWER LEVELS OF THAT SPACESUIT IS THE BLADDER ITSELF, AND THAT GETS INTO ONE OF THE NEXT IMPORTANT ASPECTS OF THE SUIT, WHICH IS PROVIDING AN OXYGEN ENVIRONMENT. >> RIGHT. >> YOU’VE GOT TO BE ABLE TO BREATHE IN SPACE, AND THERE IS A 100% OXYGEN ENVIRONMENT INSIDE THE SUIT. AND AS GARY KNOWS, AND WE’VE TALKED ABOUT IT BRIEFLY BEFORE, 100% OXYGEN ENVIRONMENT IS NOT NATURAL. >> RIGHT. >> IT’S NOT WHAT WE EXPERIENCE DOWN HERE IN AMBIENT OR ONE ATMOSPHERE PRESSURE, WHERE WE GET-- WHAT IS IT, 78% NITROGEN? >> NITROGEN, YEAH, AND A LITTLE BIT OF CARBON DIOXIDE, JUST LITTLE BIT. >> JUST A TINY BIT, TINY BIT. BUT WHEN THE LOWER PRESSURES OF THE SUIT, THE SUIT PRESSURE IS 4.3 PSI WHEN WE GO ON SPACEWALKS. >> AND THAT’S ABOUT THE PRESSURE WE FEEL HERE ON EARTH? >> THE PRESSURE WE FEEL HERE ON EARTH IS 14.7. >> WHOA, OKAY, SO A LITTLE BIT LOWER. >> SO ALMOST A THIRD, A THIRD. >> WOW. >> CLOSE TO A THIRD, A FOURTH OF THAT. >> OKAY, SO WHAT WOULD THAT FEEL LIKE? WHAT’S THE NEXT COMPARABLE THING OF WHAT 4 PSI WOULD FEEL LIKE TO LIKE US HERE ON EARTH? >> OOH, THAT’S A TOUGH ONE. >> YEAH, HARD TO COMPARE, RIGHT? >> THAT’S A TOUGH ONE, BECAUSE I’VE BEEN INSIDE OF A SUIT SO I KNOW WHAT IT FEELS LIKE, BUT I HAVEN’T BEEN INSIDE SOMETHING ELSE THAT HAS THAT 4 PSI OF PRESSURE THAT I COULD DO A 1-TO-1 COMPARISON OF. I WOULD SAY PUTTING MULTIPLE GLOVES ON. >> OH, OKAY. YEAH, SO IT’S REALLY STRENUOUS ON YOUR HANDS, THEN? >> ABSOLUTELY. WHEN YOU’RE OUT-- COMPARED TO A NEAR ZERO PRESSURE ENVIRONMENT LIKE THE SPACE IS, 4.3 IS-- IT’S FATIGUING. YOU’VE GOT PRESSURE ON YOUR HANDS, YOUR BODY. TO MOVE, YOU’VE GOT 4.3 POUNDS OF PRESSURE OVER ALL OF YOUR BODY THAT YOU’RE WORKING AGAINST. >> PRETTY STIFF. >> THAT IS. COMPARE THAT TO THE RUSSIAN ORLAN. THEIR SUIT IS 5.8 PSI. THAT’S EVEN MORE DIFFICULT. >> WOW. >> YOU COMPARE THAT TO SOME OTHER SPACESUITS THAT WE’VE LOOKED AT IN THE PAST THAT ARE EVEN HIGHER PRESSURE, AND YOU CAN SEE WHY IT GETS-- WE NEED LOW PSI. AND SO 4.3 IS NOT PERFECT WITH ZERO RESISTANCE, BUT IT’S A NICE SWEET SPOT THAT OUR CREW MEMBERS ARE ABLE TO WORK, AND THOSE THAT HAVE RAN IN BOTH THE RUSSIAN SUIT AND THE AMERICAN SPACESUIT HAVE SAID, “YEAH, IT’S A LOT EASIER, THIS 4.3 PSI.” >> OKAY. >> YEAH. BUT THAT DRIVES US TO WHY THE OXYGEN’S AT 100%. AT THAT LOWER PRESSURE, WE NEED THE 100% OXYGEN. >> OH, OKAY. SO THAT’S HOW YOU COUNTER, YOU KNOW, WE’RE IN THE 14-SOMETHING PSI HERE, SO THEN-- >> LOWER OXYGEN CONCENTRATION. >> LOWER OXYGEN, OKAY. THAT MAKES-- AND THAT BRINGS US BACK TO THE PRE-BREATHING THAT WE KIND OF ALLUDED TO EARLIER. >> YES, SIR. >> YOU NEED TO KIND OF PURGE YOUR BODY OF NITROGEN, IS THAT RIGHT? >> THAT’S RIGHT. >> OKAY. >> THAT’S RIGHT, OTHERWISE THE OXYGEN TOXICITY IS THE CONCERN IF YOU DON’T GO TO THAT PREBREATHE PROTOCOL. >> OKAY, ALL RIGHT. WELL, AWESOME. THAT EXPLAINS WHY YOU NEED THE PRESSURE THAT YOU DO. OKAY. BUT I GUESS IF YOU WERE TO DROP IT ANY LOWER IT WOULD BE A LITTLE BIT HAZARDOUS TO YOUR HEALTH, RIGHT? LIKE 4.3 IS PROBABLY THE SWEET SPOT? >> 4.3 IS THE SWEET SPOT WITH WHAT OUR CURRENT SPACESUIT IS CERTIFIED TO. >> OH. >> YOU CAN ADJUST IT DIFFERENT WAYS. I MEAN, IT’S KIND OF LIKE IF YOU CHANGE THE PRESSURE, NOW YOU’VE GOT TO PLAY WITH THE OXYGEN. YOU’VE GOT TO PLAY WITH WHAT IS THE SUIT CAPABILITIES AT THAT LEVEL. 4.3 IS THE PERFECT SWEET SPOT FOR WHAT THIS SUIT IS CERTIFIED FOR. >> AH, I SEE. WHICH IS DOING WORK ON THE OUTSIDE OF THE INTERNATIONAL SPACE STATION. >> ABSOLUTELY. >> COOL, VERY COOL. SO YOU’RE OUTSIDE-- YOU ALLUDED TO THE FACT THAT WE’RE IN LOW EARTH ORBIT, RIGHT, MEANS WE’RE IN THE MICROGRAVITY ENVIRONMENT. >> YES. >> TINY BIT OF GRAVITY, NOT TOO MUCH. IS IT FAIR TO SAY A LITTLE BIT OF ATMOSPHERE, TOO? LIKE TINY, TINY BIT? >> TINY BIT. >> YEAH, THAT’S WHY WE NEED TO BOOST THE STATION EVERY ONCE IN A WHILE. >> YES. >> THERE’S LIKE A TINY LITTLE BIT OF DRAG. BUT HOW MUCH ARE WE PROTECTED FROM THE EARTH’S, I GUESS, MAGNETIC SPHERE? HOW MUCH DO WE HAVE TO WORRY ABOUT RADIATION AT THAT ALTITUDE? >> YEAH, NO, ABSOLUTELY. GREAT QUESTION. AND IT’S A GREAT CONCERN. THERE’S A REASON THAT CREW MEMBERS ARE LIMITED FOR HOW LONG THEY CAN STAY UP ON THE INTERNATIONAL SPACE STATION. THAT’S ONE OF THE PLAYERS IN THERE IS THE HEALTH THEMSELF. RADIATION, I MEAN, I GUESS THE MOST HIGH LEVEL WAY TO DESCRIBE IT IS SUBATOMIC PARTICLES THAT ARE SUPERCHARGED WE GET FROM THE SUN, WE GET FROM OUTSIDE OUR MILKY WAY GALAXY, AND THAT CAN COME IN, AND THEY JUST TEAR RIGHT THROUGH YOUR DNA. AND THAT CAN BE ACUTE IF THERE’S LARGE DOSES OF RADIATION, WHICH FORTUNATELY AREN’T A CONCERN WHERE WE WORK IN LOW EARTH ORBIT. >> OH. >> BUT OVER A LONG-TERM EXPOSURE, THERE COULD BE CHRONIC EFFECTS. LIKE WHEN YOU REARRANGE THE DNA, IT CAN LEAD TO CANCER, OTHER DISEASES. SO IT’S VERY SERIOUS. WE HAVE A TEAM DEDICATED TO RADIATION AND MAKING SURE WE PROTECT OUR CREW MEMBERS. THE SPACESUIT IS DESIGNED TO PROVIDE SOME LEVEL OF PROTECTION WHEN THEY’RE OUT THERE FOR THAT LIMITED SPACEWALK ON THE INTERNATIONAL SPACE STATION. THE SPACE STATION ITSELF IS ALSO DESIGNED TO PROTECT THE CREW MEMBERS FROM CERTAIN LEVELS OF RADIATION THAT WE GET FROM SOLAR WIND FROM THE SUN. >> OKAY, ALL RIGHT, YEAH. SO I GUESS THE SUIT IS DESIGNED FOR WHAT-- FOR THAT PURPOSE. >> FOR THAT PURPOSE IN LIMITED SPACEWALKS, YEAH. >> OKAY. WELL, SO HOW IS THAT DIFFERENT FROM OTHER I GUESS EXTRAVEHICULAR SUITS? YOU KNOW, THE SUIT ITSELF HAS EVOLVED OVER TIME, RIGHT? BUT I HEARD, I THINK THE TECHNOLOGY IS SORT OF ADAPTED FROM 1970s TECHNOLOGY, AND THEN THEY JUST MADE IT A LITTLE BIT BETTER, RIGHT? >> SURE, SURE. >> YEAH. >> YEAH, SO YOU HAVE-- I MEAN, WE CAN GO RIGHT THROUGH THEM. YOU HAVE ALL THE WAY BACK FROM THE MERCURY SUITS, THE FIRST ONES WE WENT UP THERE WITH INSIDE OF THE MERCURY, AND THOSE WERE COMPLETELY DESIGNED FOR, HEY, THE CREW MEMBER IS STAYING INSIDE THIS VEHICLE. BUT IN CAS WE HAVE CABIN DEPRESSURIZATION, WE NEED THE GUYS TO HAVE A SUIT SO THAT THEY CAN EXIST FOR HOPEFULLY THE PERIOD OF TIME TO GET THE CABIN BACK PRESSURIZED. THOSE WERE EARLY SUITS. WE HAD EVEN BEFORE THAT PRESSURIZED SUITS FOR OUR PILOTS AND BALLOONISTS THAT WERE GOING HIGH ALTITUDE. >> RIGHT, YEAH, AND WE STILL DO, RIGHT? WE HAVE THE PILOTS OVER AT ELLINGTON FIELD HERE IN TEXAS THAT WEAR THOSE PRESSURIZED SUITS FOR THE WB-57s, THOSE HIGH ALTITUDE PLANES. >> YEP, YEP. >> SO THEY’RE, I GUESS-- ARE THEY TECHNICALLY IN SPACE AT THAT ALTITUDE? I THINK THEY ARE, RIGHT? IS IT 16 MILES THAT IS LIKE YOU’RE TECHNICALLY IN SPACE? >> YOU’RE GETTING BEYOND MY KNOWLEDGE HERE. >> I DON’T WANT TO GET LOST. SO MAYBE-- LISTEN-- >> YOU HEAR THINGS, BUT YEAH. BUT I KNOW THEY DO WEAR THE SUITS, AND THEY HAVE TO. THEY HAVE TO DO THE WHOLE SAME THING THAT ASTRONAUTS DO. THEY HAVE TO PREBREATHE AND ALL OF THAT KIND OF STUFF. BUT YEAH, SO-- >> THAT’S WHERE SPACESUITS STARTED FROM. >> RIGHT. >> THAT WAS THE FIRST STEPPING STONE, WAS HIGH ALTITUDE FLYING. >> YEAH. SO I GUESS THOSE MERCURY SUITS THAT YOU WERE TALKING ABOUT, IS THAT WHERE KIND OF THE LAUNCH AND ENTRY SUITS KIND OF WENT TOWARDS? WHENEVER YOU’RE LAUNCHING INTO SPACECRAFT, YOU HAVE TO WEAR A SPECIFIC SUIT IN CASE OF THAT, RIGHT, SUDDEN DEPRESSURIZATION? IS THAT LIKE THE REASON? >> SO ABSOLUTELY, THE MERCURY SUIT WAS A-- YOU KNOW, WE STAND ON THE SHOULDERS OF THOSE WHO DESIGNED THAT MERCURY SUIT. AND HE NEXT SUIT WAS GEMINI AFTER THAT, AND THE NEXT ONE AFTER THAT, AND ALL THE DAY TO APOLLO-- YES, ABSOLUTELY DO THOSE PROVIDE DATA AND INSIGHT TOWARDS THE ACES SUIT, OR THE LAUNCH AND ENTRY SUIT THAT WE’RE NOW WORKING ON FOR NEXT VEHICLES. >> OH, RIGHT. >> SO YES, DATA FROM THOSE SUITS WAS PIVOTAL TO MAKE OUR CURRENT LAUNCH AND ENTRY SUITS. I MEAN, ONE OF THE MOST-- THE GEMINI SUIT THAT CAME AFTER THE MERCURY, THAT WAS THE ONE THAT ED WHITE WENT OUT ON HIS EVA IN. THAT WAS THE MOST POLARIZING OR ONE OF THE MOST WELL KNOWN ONES THAT YOU’LL SEE IN A LOT OF THE OLD MOVIES WITH THE ALUMINIZED NYLON OUTER COVERING, WHERE IT’S ALL SHINY, AND A LOT OF ZIPPERS HERE AND THERE. >> CHROME. >> YEAH. EVERY MOVIE THAT EVER HAD SCIENCE FICTION LAID TO IT-- MY PARENTS WATCHED-- I REMEMBER SEEING THE SHINY SUITS. >> YEAH. >> AND SO THAT’S GEMINI. >> YEAH. >> TO SET THE TONE ON THAT. AND THE REASON FOR THE SHINY SUITS WAS THEY WERE IN THAT TIME-- WE HAD A LOT OF DATA, BUT THE BIG CONCERNS WERE THERMAL AND RADIATION, AS WE WERE TALKING ABOUT EARLIER. AND SO YOU’LL SEE THAT ALUMINIZED MATERIAL ON THE GEMINI SUIT EARLY ON, BECAUSE THEY REALLY WANT TO MAKE SURE THEY ARE GUYS WHO PROTECTED, SO THEY WENT ALL OUT. AS WE GOT MORE DATA AND WE FIGURED OUT WHAT WE NEEDED AND WHERE WE NEED TO GROW IN, AND WHERE WE DIDN’T NEED SO MUCH, YOU SAW THAT SHINY ALUMINUM OR NYLON, IT WENT AWAY. >> RIGHT, YEAH. AND NOW WE SEE THE WHITE SUIT. >> YOU GOT IT. >> ALL RIGHT, YEAH. AND THEN WE SAW THE FAMOUS WHITE ONES LIKE ON THE MOON, WALKING ON THE SURFACE OF THE MOON. >> THE APOLLO SUITS. >> THE APOLLO SUITS. AND THEN WE-- NOW WE HAVE THE WHITE SUITS ON THE INTERNATIONAL SPACE STATION THAT WE USE ALL THE TIME. SO KIND OF GOING THROUGH A LITTLE BIT OF THE FEATURES OF THOSE SUITS, I WANT TO-- I ALWAYS WANTED TO KNOW, WHENEVER YOU LOOK AT A SPACESUIT, THE FIRST THING, I THINK, YOUR EYES GO TO IS THAT SHIELD, THAT GOLD SHIELD. WHAT IS THAT? >> YEAH, SO THE-- I THINK THE TERM IS GOLDIZED. >> OOH. >> YES. >> I LIKE THAT. >> THAT GOLD VISOR IS LIKE BASICALLY VERY FANCY SUNGLASSES. >> COOL. >> SO THE VISOR ITSELF IF A LEXAN MATERIAL THAT YOU’LL FIND IN SOME OF YOUR HOUSEHOLD GOODS. IT IS SPECIFICALLY TO PROTECT THE CREW MEMBERS’ EYES FROM SUN. >> OKAY. >> AND SO THERE’S A GOLD SHEET THAT GOES OVER THAT. IT HAS GREAT CHARACTERISTICS OF BLOCKING HARMFUL UV RAYS AND OTHER RAYS THAT WOULD COME FROM THE SUN, AND HELP THE ASTRONAUT CONTINUE TO BE ABLE TO WORK IN THAT SPACEWALK ENVIRONMENT. >> BUT THEY CAN KIND OF PULL IT UP, RIGHT, DURING NIGHTTIMES. IT’S LIKE SUNGLASSES ARE. IF YOU WALK FROM OUTSIDE TO INSIDE AND IT’S SUDDENLY DARK, YOU TAKE YOUR SUNGLASSES OFF. SO IT’S KIND OF-- >> SURE, THEY’VE GOT A COOL KNOB ON THE SIDE OF THE HELMET. YOU JUST FLIP THAT VISOR UP, AND WHAT YOU REALLY NEAT IS THERE ARE OPAQUE VISORS ON THE SIDE THAT WE RARELY SEE IN PICTURES. >> RIGHT. >> MOST PICTURES YOU WANT TO SEE THE FACE OR AT LEAST THE COOL GOLD VISOR. BUT THERE ARE COMPLETELY OPAQUE WHITE VISORS THAT CAN COVER-- MAYBE IF THE SUN’S ON YOUR RIGHT SIDE, IT CAN BLOCK ON THE RIGHT, OR THE LEFT, OR HALFWAY DOWN THE FRONT. AND THEN THE GOLD VISOR, AS YOU POINTED OUT, CAN COMPLETELY COVER YOUR FACE AT FULL SUN, OR PARTIALLY, OR JUST COMPLETELY REMOVE IT ALL TOGETHER. SLIDES BACK BEHIND THE HELMET BUBBLE UNDERNEATH. OH, OKAY. OH, SO I’M THINKING ABOUT THE PICTURE OF-- I WANT TO SAY IT’S ON APOLLO 17, RIGHT, WHERE YOU HAVE THE-- I THINK IT WAS GENE CERNAN, I THINK, POSING, AND THEN HE HAS TWO OF THOSE OPAQUE VISORS DOWN-- >> AH, NOW I’M WITH YOU, YEAH. >> YEAH, AND HE’S GOT THE EARTH BEHIND HIM OR SOMETHING. >> YOU GOT IT, YOU GOT IT. >> I’M THINKING ABOUT THAT PICTURE RIGHT NOW. SO IF YOU DON’T KNOW THAT PICTURE, GO LOOK THAT ONE UP, BECAUSE THAT’S WHAT HE’S TALKING ABOUT WITH THESE OPAQUE VISORS. IT’S LIKE THOSE WHITE SHIELDS THAT COME DOWN ON THE SIDES. >> ABSOLUTELY. >> COOL. >> AND THE APOLLO SUITS ARE THE FIRST SUITS WITH THAT FAMOUS FISHBOWL TYPE HELMET. REMEMBER THAT? IF YOU LOOK AT YOUR EARLIER SUITS, THEY HAVE ROUND VISORS THAT ARE FIXED, BUT THEY’RE MORE OVAL OR SMALLER IN SHAPE, SO IT’S LIMITED VIEW. IN THE APOLLO SUITS, AND YOU’LL SEE IT ON THE CURRENT SUITS ON THE STATION, YOU HAVE THE FULL FISHBOWL HELMETS SO YOU CAN ALMOST HAVE A COMPLETE VIEW SIDE TO SIDE IN FRONT, A LITTLE ABOVE, LIMITED BELOW BY THE NECK RING, BUT A MUCH BIGGER FIELD OF VIEW FROM THE APOLLO AND THE CURRENT SUITS WE HAVE TODAY. >> AND THAT SOUNDS LIKE THE PERFECT REASON TO DO IT, RIGHT-- THEY LEARNED. THEY SAID, “ALL RIGHT, I WOULD LIKE TO HAVE A BIGGER FIELD OF VIEW,” SO THEY DESIGNED A HELMET AND THEN WENT, “OKAY, NOW I CAN SEE A LOT MORE.” SO WHAT’S THE-- I KNOW THAT ONE OF THE THINGS THAT I ALWAYS WANTED TO ASK IS I’M SURE-- YOU’RE OUTSIDE DOING A SPACEWALK FOR HOURS, RIGHT. YOUR NOSE HAS TO GET ITCHY. >> MAN, YOU KNEW YOUR NOSE WOULD GET ITCHY. [ LAUGHTER ] >> HOW DO YOU-- LIKE WHAT IF YOU JUST FEEL AN ITCH? LIKE, WHERE DO YOU GO? >> YEAH, SO-- >> DON’T THEY HAVE LIKE VELCRO OR SOMETHING? LIKE HARD VELCRO THEY CAN SCRUB THEIR NOSE ON OR SOMETHING? >> SO THERE ARE. THERE IS SOMETHING CALLED A VALSALVA. IT’S A STRANGE NAME, BUT IT’S KIND OF A-- NOT TO GET TOO INTO THE DETAILS-- IT’S A FOAM BLOCK THAT’S FIXED INSIDE THE HELMET ON THE NECK RING. >> OKAY. >> NOW, THE PURPOSE OF THIS ITEM THAT’S CALLED A VALSALVA IS FOR WHEN YOU’RE GOING THROUGH PREBREATHE AND YOU’RE PRESSURIZING THE SUIT BEFORE GOING OUT THE DOOR. LIKE WHEN YOU GO UP IN AN AIRPLANE, ONCE THAT CABIN STARTS PRESSURIZING, YOUR EARS CAN POP. THAT’S UNCOMFORTABLE. FOR US FLYING IN A PLANE, AND ESPECIALLY FOR SOMEONE INSIDE OF A SPACESUIT. ONLY THEY CAN’T GRAB THEIR NOSE AND BLOW THE AIR OUT TO EQUAL THE PRESSURIZATION. SO THEY HAVE THESE VALSALVAS THEY CAN FIT ON THEIR NOSE, AND THEY CAN KIND OF-- IT SERVES THE PURPOSE OF BLOCKING THE NASAL PASSAGE SO THEY CAN MAKE SURE THAT THEIR EARS DON’T POP. >> OH! >> SO YOU CAN SWALLOW, OR YOU CAN PUSH DOWN YOUR NOSE ON THIS BLOCK TO EQUALISE THE PRESSURE THERE. AND ALL THAT LONG STORY TO SAY, IF YOU CAN REACH YOUR NOSE DOWN THERE AND SCRATCH ON THAT BLOCK, THAT COULD BE AN OPTION, OTHERWISE YOU’RE OUT OF LUCK. >> YEAH, YEAH. WELL, I DIDN’T EVEN THINK ABOUT THAT. LIKE I WAS THINKING ABOUT ITCHY NOSE, BUT OF COURSE-- WHAT IF YOUR EARS HAVE TO POP? NOW YOU HAVE A THING TO DO THAT, TOO. >> ABSOLUTELY. >> THAT’S PRETTY COOL. >> LIKE YOU SAID EARLIER, IT’S THROUGH THESE GENERATIONS OF SUIT EVOLUTION THEY’VE LEARNED ALONG THE WAY, WITH GREAT CREW FEEDBACK OF “HEY, WE NEED THIS.” >> YEAH, YEAH, EXACTLY. WELL, YEAH. YOU’VE BEEN DOING-- THE FIRST SPACEWALK WAS, WE SAID, IN 1965. SO YOU HAVE A LOT TO LEARN FROM THE MID-60s TO NOW, OBVIOUSLY. SO WHAT ABOUT LIKE-- I MEAN, AGAIN, THINKING ABOUT YOU’RE OUTSIDE FOR THAT LONG. WHEN DO YOU EAT? DO YOU EAT LIKE RIGHT BEFOREHAND? LIKE BEFORE OR AFTER THE PREBREATHE? LIKE, I WOULD JUST GET SO HUNGRY. I HAVE TO EAT LIKE EVERY TWO TO THREE HOURS. >> I’M WITH YOU, GARY. THAT’S PROBABLY THE ONLY REASON WE’RE NOT ASTRONAUTS-- WE’VE GOT TO EAT EVERY TWO OR THREE HOURS. >> THAT WOULD BE, HONESTLY-- EVERYTHING ELSE I QUALIFY FOR, OBVIOUSLY, BUT I HAVE TO EAT EVERY TWO OR THREE HOURS, OR I CAN’T. [ LAUGHTER ] >> SO I WOULD SAY THAT’S CREW MEMBER SPECIFIC, WHERE YOU SEE AS-- I DON’T KNOW ABOUT YOU, BUT WHEN I WOULD RUN MARATHONS, I HAD FRIENDS THAT COULD EAT A BURGER BEFORE A MARATHON WITH NO PROBLEM. THAT’S NOT THIS GUY. >> NOT THIS GUY, EITHER. NO WAY. >> AND SO, SAME THING WITH CREW MEMBERS. YOU HAVE SOME THAT-- THEY HAVE A LOT OF TIME EARLIER ON WHERE IT’S RECOMMENDED, “DO NOT EAT PAST THIS TIME.” AND THERE ARE SOME THAT’LL EAT RIGHT UP ALONG THAT BARRIER, AND THERE ARE SOME THAT’LL STOP EATING WAY BEFORE THAT. BECAUSE NATURALLY, WHEN YOU EAT, NOT ONLY DOES IT SUPPLY ENERGY TO YOUR BODY, BUT IT ALSO CAUSES NORMAL BODILY FUNCTIONS AS WELL, WHICH LEADS INTO ANOTHER DISCUSSION. [ LAUGHTER ] >> THAT’S RIGHT. LET’S GO INTO THAT ONE. [ LAUGHTER ] YEAH, SO, SEVEN HOURS. AGAIN, YOU’RE OUT THERE FOR A LONG TIME. YOU’VE GOT TO GO TO THE BATHROOM. >> THAT’S RIGHT. >> WHAT DO THEY DO? >> YEAH, THAT’S A CALL THAT YOU HAVE TO ANSWER. >> RIGHT, RIGHT. >> SO UNFORTUNATELY, AS WE SAID EARLIER, WHEN YOU’RE OUT IN A SPACEWALK, YOU CAN’T JUST SAY, “HEY JOHN, I’M GOING TO HEAD INSIDE AND HIT THE JOHN.” YOU’RE STUCK OUT THERE FOR THE DURATION. >> OH, YEAH. AND EVERY MOMENT IS PLANNED, RIGHT? >> THAT’S RIGHT. >> SO YOU CAN’T-- YOU HAVE TO JUST DO YOUR THING. >> YES, ABSOLUTELY. AND SO THERE IS NO TOILET INSIDE THE SUIT. THEY HAVE-- AN ACRONYM WOULD BE THE MAG, AND IT’S BASICALLY AN ABSORPTION GARMENT. >> AS IN MAXIMUM? >> YOU’VE GOT IT, MY FRIEND. >> ALL RIGHT! >> YOU’VE GOT IT, YOU’VE GOT IT. >> BRING THAT ABSORBENCY UP TO MAXIMUM. >> SO IT’S BASICALLY A VERY LARGE DEPENDS DIAPER THAT THEY’LL WEAR ON THESE SPACEWALKS. NOW, I CAN TELL YOU, ANYONE WHO’S BEEN INSIDE A SUIT HAS ZERO DESIRE TO USE THAT DIAPER. >> YES, I CAN IMAGINE. >> ABSOLUTELY. BUT EVERY SINGLE ONE OF THEM IS GLAD IT’S THERE IF THEY GET THAT CALL. >> YES, YEAH. OKAY, YEAH. I COULD TOTALLY SEE THAT. AND THERE’S WATER, TOO, IN THE SUIT IN CASE YOU GET THIRSTY? >> ABSOLUTELY. SAME THING WITH THE MARATHON-- YOU’VE GOT TO HAVE HYDRATION, AND SO THEY HAVE WHAT THEY CALL DISPOSABLE IN SUIT DRINK BAGS. SITS RIGHT HERE ON THE CHEST, ACTUALLY VELCROS TO THE LIQUID COOLING VENTILATION GARMENT, WHICH IS HOW THEY GET THE COOLANT INSIDE THE SUIT. >> AH. >> OVER 300 FEET OF LITTLE TUBES RUN OVER THEIR ENTIRE BODY THAT CAN PROVIDE WARM OR COLD WATER THAT THE CREW MEMBER CAN ADJUST AS THEY PREFER ON A TEMPERATURE CONTROL VALVE. >> IT’S LIKE A SPACE VERSION OF AIR CONDITIONING. >> THAT’S RIGHT, LOWER THERMOSTAT RIGHT THERE. >> I’M TOO COLD. I’M JUST GOING TO TURN THE HEAT UP. OH, YEAH. >> THERE YOU GO. WELL, SITTING ON TOP OF THAT IS THAT BAG WITH WATER. >> YEAH. >> AND THEY’LL TAKE OUT 32-ISH OUNCES OF WATER AS SUITS THEM. >> OKAY, ALL RIGHT. SO THEY HAVE A LOT OF THE THINGS THAT THEY NEED. OBVIOUSLY YOU HAVE TO PLAN FOR THAT IF YOU’RE GOING TO GO OUT IN SPACE FOR THAT LONG. THAT MAKES A LOT OF SENSE. SO LET’S SEE. HOW MUCH DO THEY WEIGH? THAT’S A BIG QUESTION, RIGHT? >> A BIG QUESTION, AND BIG WEIGHT. >> YEAH. >> SO EVERY SUIT THAT’S AN EMU-- HERE I AM WITH ACRONYMS AGAIN-- THE SPACESUIT THAT OUR CREW MEMBERS USE, OUR U.S. CREW MEMBERS USE IS DESIGNED TO FIT FROM THE 5th PERCENTILE UP TO THE 95th PERCENTILE OF MEN AND WOMEN. AND SO WITH THAT, YOU HAVE CERTAIN COMPONENTS THAT ARE INTERCHANGEABLE AND DO NOT CHANGE. WHAT I MEAN BY THAT IS LIKE THE HARD UPPER TORSO-- PICTURE THE TORSO OF THE SUIT. >> YES. >> YOU’VE GOT THREE SIZES, AND THE MAJORITY OF CREW MEMBERS MIGHT USE A LARGE, FOR EXAMPLE. AND THEY SHARE THAT LARGE BETWEEN THEM. BUT ALL THE PIECES THAT CONNECT TO THE SUIT, THE ARMS, THE GLOVES, THE BOOTS, THOSE CAN ADJUST IN SIZE. AND SO IF IT’S A SMALLER SIZE IT’S GOING TO WEIGH LESS. IF IT’S A LARGER SIZE, IT’LL WEIGH MORE. BUT OVERALL, THE AVERAGE WEIGHT OF A SPACESUIT ITSELF IS ABOUT 270 POUNDS. >> WOW! >> YEAH. >> OKAY, THAT’S PRETTY HEAVY. WELL, ON EARTH, RIGHT? SO IT’S GOT SOME WEIGHT. SO HOW WOULD-- I GUESS 300 POUNDS IN SPACE WOULD BE NOT SO HARD TO MOVE AROUND, RIGHT? I GUESS YOU’RE IN THE MICROGRAVITY ENVIRONMENT. BUT LIKE WE WERE TALKING ABOUT EARLIER, IT’S THAT PRESSURE. IT’S THE PRESSURE INSIDE WHERE YOU HAVE THE GLOVES AND YOU’RE TRYING TO SQUEEZE YOUR HANDS, AND THAT’S KIND OF THE HARD PART. >> SURE. YEAH, WHAT CAN BE OUR FRIEND AT TIMES IS MOMENTUM OR INERTIA. AND THAT CAN BE AN ENEMY AT TIMES AS WELL, WHEN YOU’RE IN THAT MICRO ENVIRONMENT. SO CREW MEMBERS ARE TRAINED SPECIFICALLY TO GO SLOW ALONG A SPACE STATION. IF YOU GET 300 POUNDS MOVING, IT CAN BE DIFFICULT TO STOP. NOW, THEY CAN STOP IT, BUT IT’S JUST WASTED ENERGY. SO THEY GO VERY SLOWLY SO THEY DON’T GET THAT LARGE MASS MOVING TOO QUICKLY. >> I’D ASSUME IT ALSO HELPS WITH CONSERVING ENERGY, TOO, RIGHT? >> THAT’S RIGHT. >> SO NOT ONLY DO YOU CONSIDER AND MAKE SURE YOU CAN HAVE CONTROLLED MOVEMENT, AND YOU’RE GOING THE RIGHT PACE, AND YOU DON’T FLY EVERYWHERE, USING THAT LIMITED AMOUNT OF ENERGY BECAUSE YOU’RE CARRYING EVERYTHING WITH YOU, RIGHT? WHEN WE TALKED ABOUT THE NEUTRAL BUOYANCY LABORATORY, YOU HAVE UMBILICALS THAT HOOK UP TO ALL THE OXYGEN AND EVERYTHING YOU WANT, BUT YOU ONLY HAVE A LIMITED AMOUNT WITH YOU. BECAUSE IT’S LIKE BACKPACKING, IN SPACE, WITH A LOT MORE TECHNOLOGY. >> YES, YES. >> BUT YEAH, SO YOU REALLY HAVE TO CONSERVE. YOU HAVE TO MAKE SURE-- YOU HAVE A LIMITED AMOUNT OF OXYGEN, SO YOU HAVE TO BREATHE SLOWLY AND MAKE SURE YOUR HEART RATE’S NOT GOING UP, YOU’RE CALM WHEN YOU’RE DOING IT. >> GREAT POINT. >> YEAH, OKAY. BECAUSE I REMEMBER LISTENING WHEN WE WERE ON THE EVA, DOING THE EVA-- LIKE I WAS SAYING, THE SPACEWALK. >> THERE YOU GO WITH YOUR ACRONYMS. >> WE WERE DOING THE SPACEWALK JUST A COUPLE WEEKS AGO, AND YEAH, THEY WERE SAYING YOU’VE GOT TO MAKE SURE YOU TAKE YOUR TIME WHEN YOU’RE MOVING AROUND. BECAUSE YOU’RE OUT THERE FOR-- PLAN SIX AND A HALF, IT CAN GO UP TO SEVEN. LAST TIME IT WAS SEVEN HOURS, FOUR MINUTES. IT CAN GO UP TO EIGHT, AND I THINK THE LONGEST SPACEWALK EVER WAS ALMOST NINE. IT WAS LIKE 8 HOURS, 52 MINUTES OR SOMETHING LIKE THAT. >> IT WAS CLOSE. >> THAT’S A LONG TIME TO BE OUT THERE, AND YOU’VE GOT TO MAKE SURE YOU’RE CONSERVING THAT ENERGY. SO LET’S TALK ABOUT-- YOU BRIEFLY MENTIONED THAT THIS IS WHAT THE EMU IS MEANT TO DO, AND WE WERE TALKING ABOUT YOU GET CERTIFIED TO DO THIS, THAT-- WHAT’S HAPPENING NOW TO DESIGN FUTURE SUITS? ESPECIALLY NOT-- BECAUSE THE INTERNATIONAL SPACE STATION IS GOING TO BE THERE FOR THE NEXT HOPEFULLY DECADE, I WOULD THINK. >> SURE. >> BUT AFTER THAT WE’RE TALKING ABOUT DEEP SPACE. WE’RE TALKING ABOUT PLANETARY EXPLORATION. WHAT NEEDS TO CHANGE ABOUT THE SUIT TO MEET THOSE NEEDS? >> YEAH, SO WE HAVE A LOT OF DATA ON WHAT NEEDS TO CHANGE, BUT THERE’S A LOT OF DATA THAT WE DON’T KNOW YET. >> RIGHT, BECAUSE WE HAVEN’T BEEN THERE. >> THAT’S RIGHT, SO LIKE THE PIONEERS WITH THE HIGH ALTITUDE FLYING FOUND, “HEY, MY SUIT IS ONLY DESIGNED TO GO UP AT 5,000 FEET, AND NOW I’M AT 40,000 FEET. I THINK I’M REACHING THAT ENVELOPE.” YOU NEED NEW MATERIALS. YOU NEED NEW VEHICLES. WE’RE GOING TO FIND OUT THE SAME THING WITH THE SUIT. WHAT WE DO KNOW IS THAT THE CURRENT SPACESUIT THAT SERVES FANTASTICALLY AT THE INTERNATIONAL SPACE STATION IS NOT A PLANETARY SUIT. MOBILITY WILL BE AN ISSUE. IT IS NOT MEANT TO WALK IN IN A GRAVITY ENVIRONMENT. THINGS WE’LL HAVE TO LOOK INTO IS-- EVEN THE APOLLO SUIT, WHICH WAS LIGHTER, A LITTLE MORE FLEXIBLE, HAD SOME DESIGN CHARACTERISTICS TO ALLOW THE CREW MEMBERS TO STOOP DOWN AND PICK UP ROCKS WHERE THE CURRENT SUIT COULDN’T. EVEN THAT SUIT, THERE WAS LEARNING OPPORTUNITIES THERE WHERE THEY DIDN’T EXPECT THE AMOUNT OF DUST AND DIRT THAT WOULD COME IN AND GET INSIDE ALL THE SEALS. AND IT SOUNDS MINOR, BUT CLEANLINESS CAN HAVE CATASTROPHIC RESULTS IF YOU DON’T HAVE A CERTAIN LEVEL OF CLEANLINESS. >> THAT’S RIGHT. THEY’RE TINY LITTLE THINGS. >> THAT’S RIGHT. IF THEY GET INSIDE SEAL AND SURFACES, YOU COULD HAVE A LEAK, AND A LEAK IS SOMETHING THAT YOU DO NOT WANT WHEN YOU’RE OUT DOING A SPACEWALK. SO THERE ARE-- THE SHORT ANSWER IS OUR CURRENT SUITS ARE CERTIFIED FOR THE LOW EARTH ENVIRONMENT, FROM RADIATION REQUIREMENTS, TO THERMAL REQUIREMENTS, TO-- YOU DON’T REALLY NEED MOBILITY IN YOUR LOWER HALF. YOU JUST NEED YOUR UPPER BODY TO BE ABLE TO MOVE. REMEMBER, YOUR HANDS ARE SOME OF THE MOST IMPORTANT TOOLS YOU HAVE ON SPACE STATION. YOUR FEET AND LEGS ARE NEAR USELESS. THEY GET A LITTLE BIT OF USE, BUT NOT A WHOLE LOT. WELL, PLANETARY SUITS, WE’RE GOING TO NEED LEGS AND FEET. WE’RE GOING TO NEED TO USE THEM A LOT. >> DEFINITELY. >> AS YOU WERE HITTING ON EARLIER, AT THE LUNAR ACTIVITIES, WE’RE ONLY FOR A COUPLE OF DAYS. BUT IF WE GO TO MARS, AND IF WE LAND ON MARS, WE’RE GOING TO BE OUT THERE FOR A LOT MORE THAN A COUPLE OF DAYS. SO WE NEED A SUIT THAT’S ROBUST ENOUGH TO SUPPORT THOSE REQUIREMENTS. >> OKAY, SO I HAVE-- I’M SURE YOU’VE SEEN THE MOVIE “THE MARTIAN,” RIGHT? >> I HAVE! >> YEAH, IT’S A GOOD MOVIE. IT’S A GOOD MOVIE. SO IN THAT ONE, WHEN WE TALKED ABOUT A PLANETARY SUIT, THEY HAD THOSE LIKE SKINTIGHT ORANGE THINGS. THEY LOOKED SUPER COOL. >> AWESOME SUITS. >> YEAH, THEY LOOKED AWESOME. BUT THEN WHEN THEY WERE UP ORBITING MARS, AND THEY HAD THAT WHOLE-- I DON’T WANT TO-- IN CASE ANYONE HASN’T SEEN IT-- >> SPOILER ALERT. >> WHICH, IF YOU HAVEN’T SEEN IT, WHAT’S WRONG WITH YOU? YOU NEED TO SEE IT. BUT THEY HAD-- WHEN THEY WERE ORBITING EARTH, THEY HAD THE EMU. THEY HAD THAT BIG WHITE SUIT. AND THEN IT GOT A LITTLE TIGHTER, SKINTIGHT. IS THERE A CHANCE THAT MAYBE A PLANETARY SUIT WOULD BE SKINTIGHT, OR DO YOU NEED THOSE EXTRA LAYERS? >> SO YEAH, GREAT QUESTION. IT DEPENDS ON WHAT PLANET WE GO TO. >> OKAY. >> I MEAN, YOU HIT ON EARLIER THAT THERE’S A LITTLE BIT OF ATMOSPHERE IN THE LOW EARTH ORBIT THAT PROTECTS THE STATION TO A CERTAIN EXTENT AND CAUSES DRAG. WELL, ON MARS THERE’S ATMOSPHERE, AS WELL, WHEREAS OTHER PLANETS OR OTHER MOONS AROUND OTHER PLANETS THAT MAYBE IN THE FUTURE WE’LL LOOK AT GOING TO, WILL HAVE NEAR ZERO ATMOSPHERE. THAT’S WHERE YOU’LL NEED THE MULTIPLE LAYERS, LIKE IN OUR EMU RIGHT NOW. WHEN YOU HAVE THAT VERY MINIMAL ATMOSPHERE. M>> OKAY. >> THE MARS, WE SHOULD HAVE MORE OF AN ATMOSPHERE. WHAT YOU WANT THERE-- WHERE WE MAY GET TO MORE MULTIPLE LAYERS IS IF WE NEED A-- IF THE TECHNOLOGY IS NOT AVAILABLE TO HAVE ROBUSTNESS IN A SKINTIGHT SUIT, THEN YOU’LL GET THE MULTIPLE LAYERS. >> OH, OKAY. >> BECAUSE OBVIOUSLY YOU DON’T WANT A SUIT THAT’S GOING TO WEAR OUT AND GET A HOLE SOONER. THEN YOU’RE IN TROUBLE OUT THERE. >> RIGHT. >> BUT ABSOLUTELY, THOSE SKINTIGHT SUITS LIKE MATT DAMON HAD IN “THE MARTIAN,” AND THERE’S EVEN BEEN SOME PLAYED AROUND WITH HERE IN THE U.S. THAT WE’VE DONE SOME STUDIES FOR ADVANCED SUITS. THOSE ARE BY FAR PREFERRED IN THE ASPECTS OF MOBILITY. YOU CAN MOVE AROUND IN THOSE A LOT EASIER WITHOUT GETTING PAIN OR ABRASION FROM MULTIPLE LAYERS RUBBING ON YOU. YOU MENTIONED BACKPACKING EARLIER. WELL, IF YOU HAD A COUPLE PAIRS OF JEANS ON AT ONE TIME, AND THEN A NUMBER OF SHIRTS ON, AND THEN A BACKPACK, YOU’RE GOING GET BLISTERS AND PAIN IN PLACES. YOU DON’T WANT TO FEEL THAT. THAT’S THE TRADE OFF FOR IF YOU GET A SUIT WITH A LOT OF LAYERS OF INSULATION AND WHATNOT, AND THEN YOU TRY TO WALK DISTANCES. THAT’S GOING TO BE UNCOMFORTABLE. >> YEAH. IF THEY DO, THEY’LL PROBABLY HAVE TO DO SHORT EVAs, OR SPACEWALKS. >> OR A LUNAR ROVER. >> OH, THAT’S WHERE THE ROVER COMES IN. SO I’VE SEEN THEY HAVE ONE HERE AT THE JOHNSON SPACE CENTER CALLED THE SUV. IT’S LIKE AN ANALOG. THEY SEE-- IT LOOKS VERY MUCH LIKE THE ONE THAT WAS IN “THE MARTIAN.” IN FACT, “THE MARTIAN” KIND OF COPIED US. BUT THAT’S FINE. >> I’M OKAY WITH THAT. >> IN THE BACK, THEY HAD SUITS ON THE OUTSIDE. >> YES. >> THERE’S A REASON FOR THAT, RIGHT? >> YES. >> AND THAT WAS THAT DUST THING THAT YOU WERE TALKING ABOUT A LITTLE BIT. >> YES, YES, THAT ABSOLUTELY PLAYS INTO IT. ONE OF THE COOL THINGS ABOUT THE CURRENT SUIT WE HAVE TODAY IS JUST THE LARGE PERCENTILE OF INDIVIDUALS THAT CAN FIT INTO IT. MAYBE NOT PERFECTLY, BUT THEY CAN GET INSIDE THAT SUIT, SMALL OR LARGE, AND GO OUT AND DO AN EVA, WHEREAS THE OTHER SUITS THAT ARE FIXED IN SIZING-- I’M GONNA USE-- OBVIOUSLY THE ORLAN HAS BEEN GREAT FOR MANY YEARS. NOT HITTING THAT AT ALL, JUST SHOWING THE DIFFERENCES. >> RIGHT. >> YOU CAN'T CHANGE THE CUT SIZE. I MEAN, YOU EITHER HAVE A 37 INCH TO 44 INCH CHEST, AND YOU CAN FIT IN THERE, OR YOU CAN’T. >> OH. >> AND SO THERE’S GREAT THINGS ABOUT THAT. ONE OF THE BAD THINGS ABOUT THE EMU SUIT WHERE THOSE-- IS THAT YOU DON’T GET A LOT OF SHOULDER MOVEMENT, AND IT’S A LOT LONGER TO GET IN WHEN YOU HAVE TO PUT THE SUIT TOGETHER. ON THE GROUND WITH TECH SUPPORT, WE CAN GET THEM IN THERE IN 45 MINUTES. WHEN THEY’RE ON ORBIT, IT’S DIFFICULT TO SLIDE UP INSIDE THAT HARD UPPER TORSO. ALL RIGHT, NOW I HAVE TO PUT MY GLOVES ON, HELMET ON. NOW I’VE GOT TO PUT PANTS ON. I EXPLAINED IT IN 20 SECONDS. THOSE GUYS ARE TAKING OVER AN HOUR WITH HELP, PROFESSIONALLY TRAINED PEOPLE, TO GET INSIDE THAT SUIT. >> RIGHT. >> SO YOU HIT ON THAT SUIT ON THE BACK OF THE VEHICLE. IT OPENS UP INSIDE THAT VEHICLE. YOU CAN CRAWL INTO THAT SUIT FROM INSIDE YOUR VEHICLE WITHOUT HAVING TO DEPRESSURIZE THE WHOLE VEHICLE, CLOSE THAT HATCH ON THE SUIT, AND THEN WALK RIGHT OFF THE BACK OF THE VEHICLE. >> SWEET. >> PRETTY NEAT. >> THAT’S AWESOME, BUT YOU’RE RIGHT. YOU HAVE A SIZE THING TO CONSIDER BECAUSE YOU DON’T HAVE THAT ADJUSTABLE FEATURES OF THE EMU THAT’S ON STATION RIGHT NOW. >> BUT SINCE THE EMU WAS DESIGNED, THERE IS TECHNOLOGY THAT’S ALLOWED US TO VERY QUICKLY ADJUST THE SIZE ON SOME OF THOSE FIXED SUITS THAT FORMERLY WE COULDN’T. SO THAT’S NOT AN ISSUE TODAY, ALTHOUGH IT WAS IN THE ‘80s WHEN WE DESIGNED THE EMU. >> RIGHT. WOW. THAT IS SO COOL. OKAY, ONE MORE QUESTION, AND THEN I’M GOING TO LET YOU GO. SO WE TALKED ABOUT “THE MARTIAN” AND THOSE SKINTIGHT SUITS, BUT THERE WAS ONE SCENE IN THERE THAT HE WAS KIND OF FLOATING AROUND. AND, WELL, OKAY, I’M NOT GOING TO DO ANY SPOILERS, BUT BASICALLY HE HAD TO-- HE HAD TO-- >> I HEAR SPOILER. >> OKAY, IF YOU HAVEN’T SEEN “THE MARTIAN” YET, TURN OFF THE PODCAST. I’LL GIVE YOU THREE SECONDS. ONE, TWO, THREE. OKAY, SO HE POKES A HOLE IN HIS GLOVE ON THE OUTSIDE, AND HE HAS TO PROPEL HIMSELF OUT INTO THE THING. >> YES. >> IS THAT LIKE A THING? CAN THAT HAPPEN? I MEAN, IT PROBABLY CAN’T BE SUCCESSFUL LIKE IT WAS IN “THE MARTIAN,” BUT IS THAT A THING? IF YOU WERE TO POKE A HOLE, WOULD YOU PROPEL YOURSELF? >> SO-- MAN. SO THERE’S DEFINITELY SOME HOLLYWOOD ASPECTS TO THAT, NO DOUBT ABOUT IT. >> YES, YES. >> BUT YES, IN THEORY, YOU HAVE A PRESSURIZED SUIT. YOU’VE GOT TWO PRIMARY OXYGEN TANKS, AND THEN YOU HAVE A SECONDARY OXYGEN TANK THAT HOLDS JUST IN ITSELF ABOUT 6,000 POUNDS OF PRESSURE OF OXYGEN. SO IF YOU HAVE A HOLE AND YOU’RE PUSHING OUT AIR, EVEN IF IT’S A LOW FORCE, IT WILL GET THAT BODY MOVING. NOW, I CAN’T TELL YOU THAT IT’S GOING TO FLY YOU TO A DIFFERENT SPACECRAFT LIKE IN THE MOVIE, BUT IT WOULD BE SOME LEVEL OF PROPULSION, AND IT WOULD HELP YOU OUT. >> THAT IS SO COOL. ALL RIGHT, COOL. I JUST LOVE THAT MOVIE. THAT’S WHY I KEEP BRINGING IT UP. >> IT’S A GREAT MOVIE. >> IT’S A GOOD ONE. WELL, I THINK THAT’S ALL THE TIME WE HAVE, LES. THANK YOU SO MUCH FOR COMING ON. THIS WAS SO INTERESTING, BUT I’M SURE WE DID NOT HIT ALL OF THE POINTS ABOUT SPACESUITS. THERE’S A LOT MORE TO THIS TOPIC. >> MY HUGE BINDER WASN’T USED. >> SO IF YOU’RE LISTENING AND YOU DO HAVE QUESTIONS, MAKE SURE TO SUBMIT THEM. STAY TUNED ‘TIL AFTER THE LITTLE ENDING MUSIC CREDITS HERE, AND THEN WE’LL TALK ABOUT WHERE YOU CAN SUBMIT SOME IDEAS. AND MAYBE WE’LL DO A SPACESUITS NUMBER TWO EPISODE. WHO KNOWS. I’M SURE THERE’S MORE WE COULD TALK ABOUT. SO THANKS AGAIN, LES, AND STICK AROUND FOR MORE ON SPACESUITS. >> THANKS FOR HAVING ME, GARY. >> NO PROBLEM. ALL RIGHT. [ MUSIC ] [ INDISTINCT RADIO CHATTER ] >> WELCOME TO SPACE. >> HEY, THANKS FOR STICKING AROUND. SO TODAY WE TALKED WITH LES PADILLA ABOUT SPACESUITS. IF YOU WANT TO KNOW MORE ABOUT EVERYTHING SPACESUITS, JUST GO TO NASA.GOV/SUITUP. WE’VE GOT A NICE REFERENCE THERE FOR ALL DIFFERENT KINDS OF SPACESUITS, INCLUDING THE EMUs, MAINLY WHAT WE TALKED ABOUT TODAY. OTHERWISE, YOU CAN GO TO NASA.GOV/ISS TO LEARN ABOUT EVERYTHING GOING ON ABOARD THE INTERNATIONAL SPACE STATION. AND JUST THIS PAST MONTH IN OCTOBER, WE HAD THREE SPACEWALKS, WHERE ASTRONAUTS WERE GOING OUT IN THE EMUs TO CONDUCT SPACEWALK AND MAINTENANCE ON THE OUTSIDE OF THE STATION. YOU CAN ALSO FIND ALL THIS INFORMATION ON SOCIAL MEDIA. SO JUST GO TO FACEBOOK, TWITTER, INSTAGRAM. YOU KNOW THIS, RIGHT? WE TALK ABOUT IT ALL THE TIME. INTERNATIONAL SPACE STATION ACCOUNTS ON WHATEVER SOCIAL MEDIA PLATFORM YOU LIKE-- FACEBOOK, TWITTER, INSTAGRAM. ON FACEBOOK, INTERNATIONAL SPACE STATION. ON TWITTER IT’S @SPACE_STATION AND INSTAGRAM IS @ISS. AND IN THE BEGINNING, YOU CAN SEE THAT ALLYOOP ACTUALLY SUGGESTED THE TOPIC FOR THIS EPISODE, AND WE’RE LISTENING TO EVERYTHING YOU HAVE TO SAY. SO JUST USE THE HASHTAG #ASKNASA ON YOUR FAVORITE PLATFORM, AND SUBMIT AN IDEA FOR SOMETHING YOU’D LIKE TO HEAR ABOUT OR A QUESTION YOU’D LIKE TO ANSWER, OR MAYBE YOU’D LIKE TO FOCUS AN ENTIRE EPISODE ON ONE SPECIFIC TOPIC. SO WE’LL MAKE SURE TO LOOK AT THOSE IDEAS AND FIND THE RIGHT PERSON TO BRING ON THE SHOW. JUST MAKE SURE TO MENTION IT’S FOR HWHAP-- H-W-H-A-P-- “HOUSTON, WE HAVE A PODCAST.” THIS PODCAST WAS RECORDED ON APRIL 13, 2017. THANKS TO ALEX PERRYMAN, JOHN STOLL, AND MATT MACKENZIE. AND THANKS AGAIN TO LES PADILLA FOR COMING ON THE SHOW. WE’LL BE BACK NEXT WEEK.