Venous Gas Emboli and Ambulation at 4.3 PSIA (Preliminary)
NASA Technical Reports Server (NTRS)
Conkin, J.; Pollock, N. W.; Natoli, M. J.; Martina, S. D.; Wessel, J. H., III; Gernhardt, M. L.
2016-01-01
Ambulation imparts compressive and decompressive forces into the lower body, potentially creating quasi-stable micronuclei that influence the outcome of hypobaric depressurizations. Hypotheses: ambulation before the conclusion of a denitrogenation (prebreathe) protocol at 14.7 pounds per square inch absolute is not sufficient to increase the incidence of venous gas emboli (VGE) at 4.3 pounds per square inch absolute but is sufficient if performed after tissues become supersaturated with nitrogen at 4.3 pounds per square inch absolute.
Calculated Condenser Performance for a Mercury-Turbine Power Plant for Aircraft
NASA Technical Reports Server (NTRS)
Doyle, Ronald B.
1948-01-01
As part of an investigation af the application of nuclear energy to various types of power plants for aircraft, calculations have been made to determine the effect of several operating conditions on the performance of condensers for mercury-turbine power plants. The analysis covered 8 range of turbine-outlet pressures from 1 to 200 pounds per square inch absolute, turbine-inlet pressures from 300 to 700 pounds per square inch absolute,and a range of condenser cooling-air pressure drops, airplane flight speeds, and altitudes. The maximum load-carrying capacity (available for the nuclear reactor, working fluid, and cargo) of a mercury-turbine powered aircraft would be about half the gross weight of the airplane at a flight speed of 509 miles per hour and an altitude of 30,000 feet. This maximum is obtained with specific condenser frontal areas of 0.0063 square foot per net thrust horsepower with the condenser in a nacelle and 0.0060 square foot per net thrust horsepower with the condenser submerged in the wings (no external condenser drag) for a turbine-inlet pressure of 500 pounds per square inch absolute, a turbine-outlet pressure of 10 pounds per square inch absolute, and 8 turbine-inlet temperature of 1600 F.
46 CFR 64.11 - Design of MPTs.
Code of Federal Regulations, 2014 CFR
2014-10-01
... cargo that has a vapor pressure of 43 pounds per square inch absolute (psia) or less at a temperature of... pressure of not less than 20 pounds per square inch gauge (psig) but not more than 48 psig; and (f) To...
46 CFR 64.11 - Design of MPTs.
Code of Federal Regulations, 2011 CFR
2011-10-01
... cargo that has a vapor pressure of 43 pounds per square inch absolute (psia) or less at a temperature of... pressure of not less than 20 pounds per square inch gauge (psig) but not more than 48 psig; and (f) To...
46 CFR 64.11 - Design of MPTs.
Code of Federal Regulations, 2013 CFR
2013-10-01
... cargo that has a vapor pressure of 43 pounds per square inch absolute (psia) or less at a temperature of... pressure of not less than 20 pounds per square inch gauge (psig) but not more than 48 psig; and (f) To...
46 CFR 64.11 - Design of MPTs.
Code of Federal Regulations, 2012 CFR
2012-10-01
... cargo that has a vapor pressure of 43 pounds per square inch absolute (psia) or less at a temperature of... pressure of not less than 20 pounds per square inch gauge (psig) but not more than 48 psig; and (f) To...
33 CFR 154.2250 - General requirements.
Code of Federal Regulations, 2014 CFR
2014-07-01
... zero gas and a span gas not more than 24 hours before each cleaning operation; (5) The analyzers required by 33 CFR 154.2105(j) and 154.2107 may be checked for calibration response by use of a zero gas... cargo tank cannot be less than 14.5 pounds per square inch absolute (psia) (−0.2 pounds per square inch...
NASA Technical Reports Server (NTRS)
Wear, Jerrold D; Butze, Helmut F
1954-01-01
The effects of combustor operation at conditions representative of those encountered in high pressure-ratio turbojet engines or at high flight speeds on carbon deposition, exhaust smoke, and combustion efficiency were studied in a single tubular combustor. Carbon deposition and smoke formation tests were conducted over a range of combustor-inlet pressures from 33 to 173 pounds per square inch absolute and combustor reference velocities from 78 to 143 feet per second. Combustion efficiency tests were conducted over a range of pressures from 58 to 117 pounds per square inch absolute and velocities from 89 to 172 feet per second.
NASA Technical Reports Server (NTRS)
Doyle, R B
1951-01-01
An analysis was made at a flight Mach number of 1.5, an altitude of 45,000 feet, a turbine-inlet temperature of 1460 degrees R, of a mercury compressor-jet powered airplane using a nuclear reactor as an energy source. The calculations covered a range of turbine-exhaust and turbine-inlet pressures and condenser-inlet Mach numbers. For a turbine--inlet pressure of 40 pounds per square inch absolute, a turbine-exhaust pressure of 14 pounds per square inch absolute, and a condenser-inlet Mach number of 0.23 the calculated airplane gross weight required to carry a 20,000 pound payload was 322000 pounds and the reactor heat release per unit volume was 8.9 kilowatts per cubic inch. These do not represent optimum operating conditions.
Real-Gas Correction Factors for Hypersonic Flow Parameters in Helium
NASA Technical Reports Server (NTRS)
Erickson, Wayne D.
1960-01-01
The real-gas hypersonic flow parameters for helium have been calculated for stagnation temperatures from 0 F to 600 F and stagnation pressures up to 6,000 pounds per square inch absolute. The results of these calculations are presented in the form of simple correction factors which must be applied to the tabulated ideal-gas parameters. It has been shown that the deviations from the ideal-gas law which exist at high pressures may cause a corresponding significant error in the hypersonic flow parameters when calculated as an ideal gas. For example the ratio of the free-stream static to stagnation pressure as calculated from the thermodynamic properties of helium for a stagnation temperature of 80 F and pressure of 4,000 pounds per square inch absolute was found to be approximately 13 percent greater than that determined from the ideal-gas tabulation with a specific heat ratio of 5/3.
Method for releasing hydrogen from ammonia borane
Varma, Arvind; Diwan, Moiz; Shafirovich, Evgeny; Hwang, Hyun-Tae; Al-Kukhun, Ahmad
2013-02-19
A method of releasing hydrogen from ammonia borane is disclosed. The method comprises heating an aqueous ammonia borane solution to between about 80-135.degree. C. at between about 14.7 and 200 pounds per square inch absolute (psia) to release hydrogen by hydrothermolysis.
Exhaust-stack nozzle area and shape for individual cylinder exhaust-gas jet-propulsion system
NASA Technical Reports Server (NTRS)
Pinkel, Benjamin; Turner, Richard; Voss, Fred; Humble, Leroy V
1943-01-01
This report presents the results of an investigation conducted on the effect of exhaust-stack nozzle area, shape, and length on engine power, jet thrust, and gain in net thrust (engine propeller plus jet). Single-cylinder engine data were obtained using three straight stacks 25, 44, and 108 inches in length; an S-shaped stack, a 90 degree bend, a 180 degree bend, and a short straight stack having a closed branch faired into it. Each stack was fitted with nozzles varying in exit area from 0.91 square inch to the unrestricted area of the stack of 4.20 square inches. The engine was generally operated over a range of engine speeds from 1300 to 2100 r.p.m, inlet-manifold pressures from 22 to 30 inches of mercury absolute, and a fuel-air ratio of 0.08. The loss in engine power, the jet thrust, and the gain in net thrust are correlated in terms of several simple parameters. An example is given for determining the optimum nozzle area and the overall net thrust.
NASA Technical Reports Server (NTRS)
Curren, Arthur N; Cochran, Reeves P
1957-01-01
A combination sliding-ring and pressure-balancing seal capable of transferring pressurize air from stationary to rotating parts was developed and experimentally investigated at sliding velocities and cooling-air pressures up to 10,000 feet per minute and 38.3 pounds per square inch absolute, respectively. Leakage of cooling air was completely eliminated with an expenditure of balance air less than one-fourth the leakage loss of air from labyrinth seals under the same conditions. Additional cooling of the carbon-base seal rings was required, and the maximum wear rate on the rings was about 0.0005 inch per hour.
Performance of Several Conical Convergent-Divergent Rocket-Type Exhaust Nozzles
NASA Technical Reports Server (NTRS)
Campbell, C. E.; Farley, J. M.
1960-01-01
An investigation was conducted to obtain nozzle performance data with relatively large-scale models at pressure ratios as high as 120. Conical convergent-divergent nozzles with divergence angles alpha of 15, 25, and 29 deg. were each tested at area ratios of approximately 10, 25, and 40. Heated air (1200 F) was supplied at the nozzle inlet at pressures up to 145 pounds per square inch absolute and was exhausted into quiescent air at pressures as low as 1.2 pounds per square inch absolute. Thrust ratios for all nozzle configurations are presented over the range of pressure ratios attainable and were extrapolated when possible to design pressure ratio and beyond. Design thrust ratios decreased with increasing nozzle divergence angle according to the trend predicted by the (1 + cos alpha)/2 parameter. Decreasing the nozzle divergence angle resulted in sizable increases in thrust ratio for a given surface-area ratio (nozzle weight), particularly at low nozzle pressure ratios. Correlations of the nozzle static pressure at separation and of the average static pressure downstream of separation with various nozzle parameters permitted the calculation of thrust in the separated-flow region from unseparated static-pressure distributions. Thrust ratios calculated by this method agreed with measured values within about 1 percent.
21 CFR 177.2550 - Reverse osmosis membranes.
Code of Federal Regulations, 2014 CFR
2014-04-01
... maximum weight is 62 milligrams per square decimeter (4 milligrams per square inch) as a thin film... square decimeter (0.3 milligrams per square inch) as a thin film composite on a suitable support. The... square decimeter (0.03 milligrams per square inch). (3) For the purpose of this section, the reverse...
46 CFR 32.60-40 - Construction and testing of cargo tanks and bulkheads-TB/ALL.
Code of Federal Regulations, 2010 CFR
2010-10-01
... cargo tanks vented at gage pressure of 4 pounds per square inch or less shall be constructed and tested... 4 pounds per square inch but not exceeding 10 pounds per square inch gage pressure will be given... square inch are considered to be pressure vessels and shall be of cylindrical or similar design and shall...
46 CFR 32.60-40 - Construction and testing of cargo tanks and bulkheads-TB/ALL.
Code of Federal Regulations, 2013 CFR
2013-10-01
... cargo tanks vented at gage pressure of 4 pounds per square inch or less shall be constructed and tested... 4 pounds per square inch but not exceeding 10 pounds per square inch gage pressure will be given... square inch are considered to be pressure vessels and shall be of cylindrical or similar design and shall...
46 CFR 32.60-40 - Construction and testing of cargo tanks and bulkheads-TB/ALL.
Code of Federal Regulations, 2012 CFR
2012-10-01
... cargo tanks vented at gage pressure of 4 pounds per square inch or less shall be constructed and tested... 4 pounds per square inch but not exceeding 10 pounds per square inch gage pressure will be given... square inch are considered to be pressure vessels and shall be of cylindrical or similar design and shall...
46 CFR 32.60-40 - Construction and testing of cargo tanks and bulkheads-TB/ALL.
Code of Federal Regulations, 2011 CFR
2011-10-01
... cargo tanks vented at gage pressure of 4 pounds per square inch or less shall be constructed and tested... 4 pounds per square inch but not exceeding 10 pounds per square inch gage pressure will be given... square inch are considered to be pressure vessels and shall be of cylindrical or similar design and shall...
46 CFR 32.60-40 - Construction and testing of cargo tanks and bulkheads-TB/ALL.
Code of Federal Regulations, 2014 CFR
2014-10-01
... cargo tanks vented at gage pressure of 4 pounds per square inch or less shall be constructed and tested... 4 pounds per square inch but not exceeding 10 pounds per square inch gage pressure will be given... square inch are considered to be pressure vessels and shall be of cylindrical or similar design and shall...
Code of Federal Regulations, 2014 CFR
2014-01-01
... centimeter=0.393 701 in. 1 yard=0.9144m* 1 meter=3.280 84 ft. Area 1 square inch=6.4516 cm2* 1 square centimeter=0.155 000 in2. 1 square foot=929.0304 cm2* 1 square decimeter=0.107 639 ft2. =9.290 304 dm2 1 square meter=10.763 9 ft2. 1 square yard=0.836 127 m2 Volume or Capacity 1 cubic inch=16.3871 cm3 1 cubic...
Code of Federal Regulations, 2011 CFR
2011-01-01
... centimeter=0.393 701 in. 1 yard=0.9144m* 1 meter=3.280 84 ft. Area 1 square inch=6.4516 cm2* 1 square centimeter=0.155 000 in2. 1 square foot=929.0304 cm2* 1 square decimeter=0.107 639 ft2. =9.290 304 dm2 1 square meter=10.763 9 ft2. 1 square yard=0.836 127 m2 Volume or Capacity 1 cubic inch=16.3871 cm3 1 cubic...
Code of Federal Regulations, 2012 CFR
2012-01-01
... centimeter=0.393 701 in. 1 yard=0.9144m* 1 meter=3.280 84 ft. Area 1 square inch=6.4516 cm2* 1 square centimeter=0.155 000 in2. 1 square foot=929.0304 cm2* 1 square decimeter=0.107 639 ft2. =9.290 304 dm2 1 square meter=10.763 9 ft2. 1 square yard=0.836 127 m2 Volume or Capacity 1 cubic inch=16.3871 cm3 1 cubic...
Code of Federal Regulations, 2013 CFR
2013-01-01
... centimeter=0.393 701 in. 1 yard=0.9144m* 1 meter=3.280 84 ft. Area 1 square inch=6.4516 cm2* 1 square centimeter=0.155 000 in2. 1 square foot=929.0304 cm2* 1 square decimeter=0.107 639 ft2. =9.290 304 dm2 1 square meter=10.763 9 ft2. 1 square yard=0.836 127 m2 Volume or Capacity 1 cubic inch=16.3871 cm3 1 cubic...
Code of Federal Regulations, 2011 CFR
2011-10-01
... a bursting pressure of not less than 6,000 pounds per square inch. (b) All piping, in nominal sizes... square inch shall be installed in the distribution manifold or such other location as to protect the... manifold shall be subjected to a pressure of 1,000 pounds per square inch. With no additional gas being...
Code of Federal Regulations, 2012 CFR
2012-10-01
... fittings shall have a bursting pressure of not less than 6,000 pounds per square inch. (b) All piping, in...,800 pounds per square inch shall be installed in the distribution manifold or such other location as... stop valves in the manifold shall be subjected to a pressure of 1,000 pounds per square inch. With no...
Code of Federal Regulations, 2014 CFR
2014-10-01
... a bursting pressure of not less than 6,000 pounds per square inch. (b) All piping, in nominal sizes... square inch shall be installed in the distributing manifold or such other location as to protect the... manifold shall be subjected to a pressure of 1,000 pounds per square inch. With no additional gas being...
Code of Federal Regulations, 2013 CFR
2013-10-01
... fittings shall have a bursting pressure of not less than 6,000 pounds per square inch. (b) All piping, in...,800 pounds per square inch shall be installed in the distribution manifold or such other location as... stop valves in the manifold shall be subjected to a pressure of 1,000 pounds per square inch. With no...
Code of Federal Regulations, 2013 CFR
2013-10-01
... a bursting pressure of not less than 6,000 pounds per square inch. (b) All piping, in nominal sizes... square inch shall be installed in the distributing manifold or such other location as to protect the... manifold shall be subjected to a pressure of 1,000 pounds per square inch. With no additional gas being...
Code of Federal Regulations, 2011 CFR
2011-10-01
... a bursting pressure of not less than 6,000 pounds per square inch. (b) All piping, in nominal sizes... square inch shall be installed in the distributing manifold or such other location as to protect the... manifold shall be subjected to a pressure of 1,000 pounds per square inch. With no additional gas being...
Code of Federal Regulations, 2010 CFR
2010-10-01
... a bursting pressure of not less than 6,000 pounds per square inch. (b) All piping, in nominal sizes... square inch shall be installed in the distributing manifold or such other location as to protect the... manifold shall be subjected to a pressure of 1,000 pounds per square inch. With no additional gas being...
Code of Federal Regulations, 2012 CFR
2012-10-01
... a bursting pressure of not less than 6,000 pounds per square inch. (b) All piping, in nominal sizes... square inch shall be installed in the distributing manifold or such other location as to protect the... manifold shall be subjected to a pressure of 1,000 pounds per square inch. With no additional gas being...
Code of Federal Regulations, 2010 CFR
2010-10-01
... a bursting pressure of not less than 6,000 pounds per square inch. (b) All piping, in nominal sizes... square inch shall be installed in the distribution manifold or such other location as to protect the... manifold shall be subjected to a pressure of 1,000 pounds per square inch. With no additional gas being...
Code of Federal Regulations, 2014 CFR
2014-10-01
... fittings shall have a bursting pressure of not less than 6,000 pounds per square inch. (b) All piping, in...,800 pounds per square inch shall be installed in the distribution manifold or such other location as... stop valves in the manifold shall be subjected to a pressure of 1,000 pounds per square inch. With no...
46 CFR 98.25-10 - Design and construction of cargo tanks.
Code of Federal Regulations, 2012 CFR
2012-10-01
... for a pressure of not less than 250 pounds per square inch gage. (c) Where unrefrigerated cargo tanks... less than 215 pounds per square inch gage. (d) Refrigerated cargo tanks, in which the temperature of... system is to be maintained, plus 25 pounds per square inch gage. (e) Each tank shall be provided with not...
46 CFR 98.25-10 - Design and construction of cargo tanks.
Code of Federal Regulations, 2013 CFR
2013-10-01
... for a pressure of not less than 250 pounds per square inch gage. (c) Where unrefrigerated cargo tanks... less than 215 pounds per square inch gage. (d) Refrigerated cargo tanks, in which the temperature of... system is to be maintained, plus 25 pounds per square inch gage. (e) Each tank shall be provided with not...
Federal Register 2010, 2011, 2012, 2013, 2014
2010-03-01
...). ACTION: Final rule. SUMMARY: This action establishes an applicable standard of 7.8 pounds per square inch... gasoline at 7.8 pounds per square inch (psi) under the federal volatility control program in the Denver....8 7.8 * * * * * * * \\1\\ Standards are expressed in pounds per square inch (psi). \\2\\ The Colorado...
Code of Federal Regulations, 2014 CFR
2014-10-01
...-inch (8.3 cm) square stretch mesh (as measured between the centers of opposite knots when stretched taut) or 33/4-inch (9.5 cm) diamond stretch mesh for trawls and 27/8-inch (7.3 cm) stretch mesh for..., in the EEZ when using a mesh size less than 3 1/4-inch (8.3 cm) square stretch mesh (as measured...
Code of Federal Regulations, 2012 CFR
2012-10-01
...-inch (8.3 cm) square stretch mesh (as measured between the centers of opposite knots when stretched taut) or 33/4-inch (9.5 cm) diamond stretch mesh for trawls and 27/8-inch (7.3 cm) stretch mesh for..., in the EEZ when using a mesh size less than 3 1/4-inch (8.3 cm) square stretch mesh (as measured...
Code of Federal Regulations, 2013 CFR
2013-10-01
...-inch (8.3 cm) square stretch mesh (as measured between the centers of opposite knots when stretched taut) or 33/4-inch (9.5 cm) diamond stretch mesh for trawls and 27/8-inch (7.3 cm) stretch mesh for..., in the EEZ when using a mesh size less than 3 1/4-inch (8.3 cm) square stretch mesh (as measured...
46 CFR 171.145 - Drainage of a vessel with a cockpit.
Code of Federal Regulations, 2011 CFR
2011-10-01
... either of the following equations: A=0.1(D) square inches. A=6.94(D) square centimeters. Where— A = the combined area of the scuppers in square inches (square centimeters). D = the area of the cockpit in square feet (square meters). (e) The cockpit deck of a vessel that operates on exposed or partially protected...
46 CFR 171.145 - Drainage of a vessel with a cockpit.
Code of Federal Regulations, 2013 CFR
2013-10-01
... either of the following equations: A=0.1(D) square inches. A=6.94(D) square centimeters. Where— A = the combined area of the scuppers in square inches (square centimeters). D = the area of the cockpit in square feet (square meters). (e) The cockpit deck of a vessel that operates on exposed or partially protected...
46 CFR 171.145 - Drainage of a vessel with a cockpit.
Code of Federal Regulations, 2014 CFR
2014-10-01
... either of the following equations: A=0.1(D) square inches. A=6.94(D) square centimeters. Where— A = the combined area of the scuppers in square inches (square centimeters). D = the area of the cockpit in square feet (square meters). (e) The cockpit deck of a vessel that operates on exposed or partially protected...
46 CFR 171.145 - Drainage of a vessel with a cockpit.
Code of Federal Regulations, 2012 CFR
2012-10-01
... either of the following equations: A=0.1(D) square inches. A=6.94(D) square centimeters. Where— A = the combined area of the scuppers in square inches (square centimeters). D = the area of the cockpit in square feet (square meters). (e) The cockpit deck of a vessel that operates on exposed or partially protected...
46 CFR 171.145 - Drainage of a vessel with a cockpit.
Code of Federal Regulations, 2010 CFR
2010-10-01
... either of the following equations: A=0.1(D) square inches. A=6.94(D) square centimeters. Where— A = the combined area of the scuppers in square inches (square centimeters). D = the area of the cockpit in square feet (square meters). (e) The cockpit deck of a vessel that operates on exposed or partially protected...
46 CFR 108.449 - Piping tests.
Code of Federal Regulations, 2012 CFR
2012-10-01
... square centimeter (1000 pounds per square inch), with no additional gas introduced into the system, the... of more than 10.5 kilograms per square centimeter (150 pounds per square inch) per minute for a 2 minute period. (c) When tested with CO2 or other inert gas under a pressure of 42 kilograms per square...
46 CFR 108.449 - Piping tests.
Code of Federal Regulations, 2011 CFR
2011-10-01
... square centimeter (1000 pounds per square inch), with no additional gas introduced into the system, the... of more than 10.5 kilograms per square centimeter (150 pounds per square inch) per minute for a 2 minute period. (c) When tested with CO2 or other inert gas under a pressure of 42 kilograms per square...
46 CFR 108.449 - Piping tests.
Code of Federal Regulations, 2014 CFR
2014-10-01
... square centimeter (1000 pounds per square inch), with no additional gas introduced into the system, the... of more than 10.5 kilograms per square centimeter (150 pounds per square inch) per minute for a 2 minute period. (c) When tested with CO2 or other inert gas under a pressure of 42 kilograms per square...
46 CFR 108.449 - Piping tests.
Code of Federal Regulations, 2010 CFR
2010-10-01
... square centimeter (1000 pounds per square inch), with no additional gas introduced into the system, the... of more than 10.5 kilograms per square centimeter (150 pounds per square inch) per minute for a 2 minute period. (c) When tested with CO2 or other inert gas under a pressure of 42 kilograms per square...
42 CFR 84.148 - Type C supplied-air respirator, continuous flow class; minimum requirements.
Code of Federal Regulations, 2011 CFR
2011-10-01
... the hose connection shall not exceed 863 kN/m.2 (125 pounds per square inch gage). (c) Where the pressure at any point in the supply system exceeds 863 kN/m.2 (125 pounds per square inch gage), the... connection from exceeding 863 kN/m.2 (125 pounds per square inch gage) under any conditions. ...
42 CFR 84.148 - Type C supplied-air respirator, continuous flow class; minimum requirements.
Code of Federal Regulations, 2013 CFR
2013-10-01
... the hose connection shall not exceed 863 kN/m.2 (125 pounds per square inch gage). (c) Where the pressure at any point in the supply system exceeds 863 kN/m.2 (125 pounds per square inch gage), the... connection from exceeding 863 kN/m.2 (125 pounds per square inch gage) under any conditions. ...
Code of Federal Regulations, 2010 CFR
2010-10-01
... per square inch) with from 6 to 76 m. (15 to 250 feet) of air-supply hose. (c) The specified air... pounds per square inch gage). (d)(1) Where the pressure in the air-supply system exceeds 863 kN/m.2 (125 pounds per square inch gage), the respirator shall be equipped with a pressure-release mechanism that...
42 CFR 84.148 - Type C supplied-air respirator, continuous flow class; minimum requirements.
Code of Federal Regulations, 2012 CFR
2012-10-01
... the hose connection shall not exceed 863 kN/m.2 (125 pounds per square inch gage). (c) Where the pressure at any point in the supply system exceeds 863 kN/m.2 (125 pounds per square inch gage), the... connection from exceeding 863 kN/m.2 (125 pounds per square inch gage) under any conditions. ...
Code of Federal Regulations, 2011 CFR
2011-10-01
... per square inch) with from 6 to 76 m. (15 to 250 feet) of air-supply hose. (c) The specified air... pounds per square inch gage). (d)(1) Where the pressure in the air-supply system exceeds 863 kN/m.2 (125 pounds per square inch gage), the respirator shall be equipped with a pressure-release mechanism that...
42 CFR 84.148 - Type C supplied-air respirator, continuous flow class; minimum requirements.
Code of Federal Regulations, 2010 CFR
2010-10-01
... the hose connection shall not exceed 863 kN/m.2 (125 pounds per square inch gage). (c) Where the pressure at any point in the supply system exceeds 863 kN/m.2 (125 pounds per square inch gage), the... connection from exceeding 863 kN/m.2 (125 pounds per square inch gage) under any conditions. ...
Code of Federal Regulations, 2012 CFR
2012-10-01
... per square inch) with from 6 to 76 m. (15 to 250 feet) of air-supply hose. (c) The specified air... pounds per square inch gage). (d)(1) Where the pressure in the air-supply system exceeds 863 kN/m.2 (125 pounds per square inch gage), the respirator shall be equipped with a pressure-release mechanism that...
Code of Federal Regulations, 2013 CFR
2013-10-01
... per square inch) with from 6 to 76 m. (15 to 250 feet) of air-supply hose. (c) The specified air... pounds per square inch gage). (d)(1) Where the pressure in the air-supply system exceeds 863 kN/m.2 (125 pounds per square inch gage), the respirator shall be equipped with a pressure-release mechanism that...
42 CFR 84.148 - Type C supplied-air respirator, continuous flow class; minimum requirements.
Code of Federal Regulations, 2014 CFR
2014-10-01
... the hose connection shall not exceed 863 kN/m.2 (125 pounds per square inch gage). (c) Where the pressure at any point in the supply system exceeds 863 kN/m.2 (125 pounds per square inch gage), the... connection from exceeding 863 kN/m.2 (125 pounds per square inch gage) under any conditions. ...
Code of Federal Regulations, 2014 CFR
2014-10-01
... per square inch) with from 6 to 76 m. (15 to 250 feet) of air-supply hose. (c) The specified air... pounds per square inch gage). (d)(1) Where the pressure in the air-supply system exceeds 863 kN/m.2 (125 pounds per square inch gage), the respirator shall be equipped with a pressure-release mechanism that...
16 CFR 500.13 - Measurement of commodities by area measure only, how expressed.
Code of Federal Regulations, 2011 CFR
2011-01-01
... declaration of net quantity in terms of square yards, square feet, and square inches shall be expressed in the following manner: (a) If less than 1 square foot (929 cm2), in terms of square inches and fractions thereof. (b) If at least 1 square foot (929 cm2) but less than 4 square feet (37.1 dm2), in terms of square...
16 CFR 500.13 - Measurement of commodities by area measure only, how expressed.
Code of Federal Regulations, 2010 CFR
2010-01-01
... declaration of net quantity in terms of square yards, square feet, and square inches shall be expressed in the following manner: (a) If less than 1 square foot (929 cm2), in terms of square inches and fractions thereof. (b) If at least 1 square foot (929 cm2) but less than 4 square feet (37.1 dm2), in terms of square...
16 CFR 500.13 - Measurement of commodities by area measure only, how expressed.
Code of Federal Regulations, 2014 CFR
2014-01-01
... declaration of net quantity in terms of square yards, square feet, and square inches shall be expressed in the following manner: (a) If less than 1 square foot (929 cm2), in terms of square inches and fractions thereof. (b) If at least 1 square foot (929 cm2) but less than 4 square feet (37.1 dm2), in terms of square...
16 CFR 500.13 - Measurement of commodities by area measure only, how expressed.
Code of Federal Regulations, 2013 CFR
2013-01-01
... declaration of net quantity in terms of square yards, square feet, and square inches shall be expressed in the following manner: (a) If less than 1 square foot (929 cm2), in terms of square inches and fractions thereof. (b) If at least 1 square foot (929 cm2) but less than 4 square feet (37.1 dm2), in terms of square...
16 CFR 500.13 - Measurement of commodities by area measure only, how expressed.
Code of Federal Regulations, 2012 CFR
2012-01-01
... declaration of net quantity in terms of square yards, square feet, and square inches shall be expressed in the following manner: (a) If less than 1 square foot (929 cm2), in terms of square inches and fractions thereof. (b) If at least 1 square foot (929 cm2) but less than 4 square feet (37.1 dm2), in terms of square...
21 CFR 102.41 - Potato chips made from dried potatoes.
Code of Federal Regulations, 2010 CFR
2010-04-01
... area of 5 square inches or less and not less than one-eighth inch in height if the area of the principal display panel is greater than 5 square inches; or (2) Not less than one-half the height of the...
21 CFR 102.49 - Fried clams made from minced clams.
Code of Federal Regulations, 2010 CFR
2010-04-01
... packages having a principal display panel with an area of 5 square inches or less and not less than one-eighth inch in height if the area of the principal display panel is greater than 5 square inches; or (2...
21 CFR 102.45 - Fish sticks or portions made from minced fish.
Code of Federal Regulations, 2010 CFR
2010-04-01
...-sixteenth inch in height on packages having a principal display panel with an area of 5 square inches or... than 5 square inches; or (2) Not less than one-half the height of the largest type used in the words...
Accuracy analysis of the space shuttle solid rocket motor profile measuring device
NASA Technical Reports Server (NTRS)
Estler, W. Tyler
1989-01-01
The Profile Measuring Device (PMD) was developed at the George C. Marshall Space Flight Center following the loss of the Space Shuttle Challenger. It is a rotating gauge used to measure the absolute diameters of mating features of redesigned Solid Rocket Motor field joints. Diameter tolerance of these features are typically + or - 0.005 inches and it is required that the PMD absolute measurement uncertainty be within this tolerance. In this analysis, the absolute accuracy of these measurements were found to be + or - 0.00375 inches, worst case, with a potential accuracy of + or - 0.0021 inches achievable by improved temperature control.
Theoretical performance of some rocket propellants containing hydrogen, nitrogen, and oxygen
NASA Technical Reports Server (NTRS)
Miller, Riley O; Ordin, Paul M
1948-01-01
Theoretical performance data including nozzle-exit temperature, specific impulse, volume specific impulse and composition, temperature, and mean molecular weight of reaction products based on frozen equilibrium and isentropic expansion are presented for 13 propellant combinations at reaction pressure of 300 pounds per square inch absolute and expansion ratio of 20.4. On basis of maximum specific impulse alone, five fuels had the following order for any given oxidant: liquid hydrogen, hydrazine, liquid ammonia, and either hydrazine hydrate or hydroxylamine. Three oxidants with a given fuel had the following order: liquid ozone, liquid oxygen, and 100-percent hydrogen peroxide.
Altitude Starting Tests of a 1000-Pound-Thrust Solid-Propellant Rocket
NASA Technical Reports Server (NTRS)
Sloop, John L.; Rollbuhler, R. James; Krawczonek, Eugene M.
1957-01-01
Four solid-propellant rocket engines of nominal 1000-pound-thrust were tested for starting characteristics at pressure altitudes ranging from 112,500 to 123,000 feet and at a temperature of -75 F. All engines ignited and operated successfully. Average chamber pressures ranged from 1060 to ll90 pounds per square inch absolute with action times from 1.51 to 1.64 seconds and ignition delays from 0.070 t o approximately 0.088 second. The chamber pressures and action times were near the specifications, but the ignition delay was almost twice the specified value of 0.040 second.
46 CFR 108.417 - Fire pump components and associated equipment.
Code of Federal Regulations, 2012 CFR
2012-10-01
... discharge side that is set to relieve at 1.75 kilograms per square centimeter (approximately 25 pounds per square inch) in excess of the pump discharge pressure necessary to meet the pressure required in § 108.415 for the pump or 8.6 kilograms per square centimeters (approximately 125 pounds per square inch...
21 CFR 177.2550 - Reverse osmosis membranes.
Code of Federal Regulations, 2011 CFR
2011-04-01
... is on the food-contact surface, and its maximum weight is 62 milligrams per square decimeter (4 milligrams per square inch) as a thin film composite on a suitable support. (2) A cross-linked polyetheramine... weight is 4.7 milligrams per square decimeter (0.3 milligrams per square inch) as a thin film composite...
46 CFR 108.417 - Fire pump components and associated equipment.
Code of Federal Regulations, 2010 CFR
2010-10-01
... discharge side that is set to relieve at 1.75 kilograms per square centimeter (approximately 25 pounds per square inch) in excess of the pump discharge pressure necessary to meet the pressure required in § 108.415 for the pump or 8.6 kilograms per square centimeters (approximately 125 pounds per square inch...
21 CFR 177.2550 - Reverse osmosis membranes.
Code of Federal Regulations, 2013 CFR
2013-04-01
... is on the food-contact surface, and its maximum weight is 62 milligrams per square decimeter (4 milligrams per square inch) as a thin film composite on a suitable support. (2) A cross-linked polyetheramine... weight is 4.7 milligrams per square decimeter (0.3 milligrams per square inch) as a thin film composite...
46 CFR 108.417 - Fire pump components and associated equipment.
Code of Federal Regulations, 2011 CFR
2011-10-01
... discharge side that is set to relieve at 1.75 kilograms per square centimeter (approximately 25 pounds per square inch) in excess of the pump discharge pressure necessary to meet the pressure required in § 108.415 for the pump or 8.6 kilograms per square centimeters (approximately 125 pounds per square inch...
46 CFR 108.417 - Fire pump components and associated equipment.
Code of Federal Regulations, 2014 CFR
2014-10-01
... discharge side that is set to relieve at 1.75 kilograms per square centimeter (approximately 25 pounds per square inch) in excess of the pump discharge pressure necessary to meet the pressure required in § 108.415 for the pump or 8.6 kilograms per square centimeters (approximately 125 pounds per square inch...
21 CFR 177.2550 - Reverse osmosis membranes.
Code of Federal Regulations, 2010 CFR
2010-04-01
... is on the food-contact surface, and its maximum weight is 62 milligrams per square decimeter (4 milligrams per square inch) as a thin film composite on a suitable support. (2) A cross-linked polyetheramine... weight is 4.7 milligrams per square decimeter (0.3 milligrams per square inch) as a thin film composite...
21 CFR 177.2550 - Reverse osmosis membranes.
Code of Federal Regulations, 2012 CFR
2012-04-01
... is on the food-contact surface, and its maximum weight is 62 milligrams per square decimeter (4 milligrams per square inch) as a thin film composite on a suitable support. (2) A cross-linked polyetheramine... weight is 4.7 milligrams per square decimeter (0.3 milligrams per square inch) as a thin film composite...
46 CFR 108.417 - Fire pump components and associated equipment.
Code of Federal Regulations, 2013 CFR
2013-10-01
... discharge side that is set to relieve at 1.75 kilograms per square centimeter (approximately 25 pounds per square inch) in excess of the pump discharge pressure necessary to meet the pressure required in § 108.415 for the pump or 8.6 kilograms per square centimeters (approximately 125 pounds per square inch...
Code of Federal Regulations, 2012 CFR
2012-10-01
..., and fitting in a CO2 system must have a bursting pressure of at least 420 kilograms per square centimeter (6,000 pounds per square inch). (b) All piping for a CO2 system of nominal size of 19.05... between 168 and 196 kilograms per square centimeter (2,400 and 2,800 pounds per square inch) in the...
46 CFR 108.441 - Piping and discharge rates for CO2 systems.
Code of Federal Regulations, 2014 CFR
2014-10-01
... in square centimeters is determined by multiplying the factor 0.0313 by the number of kilograms of CO2 required. (The nominal cylinder outlet area in square inches is determined by multiplying the... than 71 square millimeters (0.110 square inches). (e) A CO2 system must discharge at least 85 percent...
46 CFR 108.441 - Piping and discharge rates for CO2 systems.
Code of Federal Regulations, 2010 CFR
2010-10-01
... in square centimeters is determined by multiplying the factor 0.0313 by the number of kilograms of CO2 required. (The nominal cylinder outlet area in square inches is determined by multiplying the... than 71 square millimeters (0.110 square inches). (e) A CO2 system must discharge at least 85 percent...
46 CFR 108.441 - Piping and discharge rates for CO2 systems.
Code of Federal Regulations, 2013 CFR
2013-10-01
... in square centimeters is determined by multiplying the factor 0.0313 by the number of kilograms of CO2 required. (The nominal cylinder outlet area in square inches is determined by multiplying the... than 71 square millimeters (0.110 square inches). (e) A CO2 system must discharge at least 85 percent...
Code of Federal Regulations, 2013 CFR
2013-10-01
..., and fitting in a CO2 system must have a bursting pressure of at least 420 kilograms per square centimeter (6,000 pounds per square inch). (b) All piping for a CO2 system of nominal size of 19.05... between 168 and 196 kilograms per square centimeter (2,400 and 2,800 pounds per square inch) in the...
46 CFR 108.441 - Piping and discharge rates for CO2 systems.
Code of Federal Regulations, 2012 CFR
2012-10-01
... in square centimeters is determined by multiplying the factor 0.0313 by the number of kilograms of CO2 required. (The nominal cylinder outlet area in square inches is determined by multiplying the... than 71 square millimeters (0.110 square inches). (e) A CO2 system must discharge at least 85 percent...
Code of Federal Regulations, 2010 CFR
2010-10-01
..., and fitting in a CO2 system must have a bursting pressure of at least 420 kilograms per square centimeter (6,000 pounds per square inch). (b) All piping for a CO2 system of nominal size of 19.05... between 168 and 196 kilograms per square centimeter (2,400 and 2,800 pounds per square inch) in the...
46 CFR 108.441 - Piping and discharge rates for CO2 systems.
Code of Federal Regulations, 2011 CFR
2011-10-01
... in square centimeters is determined by multiplying the factor 0.0313 by the number of kilograms of CO2 required. (The nominal cylinder outlet area in square inches is determined by multiplying the... than 71 square millimeters (0.110 square inches). (e) A CO2 system must discharge at least 85 percent...
Code of Federal Regulations, 2011 CFR
2011-10-01
..., and fitting in a CO2 system must have a bursting pressure of at least 420 kilograms per square centimeter (6,000 pounds per square inch). (b) All piping for a CO2 system of nominal size of 19.05... between 168 and 196 kilograms per square centimeter (2,400 and 2,800 pounds per square inch) in the...
Code of Federal Regulations, 2014 CFR
2014-10-01
..., and fitting in a CO2 system must have a bursting pressure of at least 420 kilograms per square centimeter (6,000 pounds per square inch). (b) All piping for a CO2 system of nominal size of 19.05... between 168 and 196 kilograms per square centimeter (2,400 and 2,800 pounds per square inch) in the...
Nonmetallic Material Compatibility with Liquid Fluorine
NASA Technical Reports Server (NTRS)
Price, Harold G , Jr; Douglass, Howard W
1957-01-01
Static tests were made on the compatibility of liquid fluorine with several nonmetallic materials at -3200 F and at pressures of 0 and 1500 pounds per square inch gage. The results are compared with those from previous work with gaseous fluorine at the same pressures, but at atmospheric temperature. In general, although environmental effects were not always consistent, reactivity was least with the low-temperature, low-pressure liquid fluorine. Reactivity was greatest with the warm, high-pressure gaseous fluorine. None of the liquids and greases tested was found to be entirely suitable for use in fluorine systems. Polytrifluorochloroethylene and N-43, the formula for which is (C4F9)3N, did not react with liquid fluorine at atmospheric pressure or 1500 pounds per square inch gage under static conditions, but they did react when injected into liquid fluorine at 1500 pounds per square inch gage; they also reacted with gaseous fluorine at 1500 pounds per square inch gage. While water did not react with liquid fluorine at 1500 pounds per square inch gage, it is known to react violently with fluorine under other conditions. The pipe-thread lubricant Q-Seal did not react with liquid fluorine, but did react with gaseous fluorine at 1500 pounds per square inch gage. Of the solids, ruby (Al2O3) and Teflon did not react under the test conditions. The results show that the compatibility of fluorine with nonmetals depends on the state of the fluorine and the system design.
40 CFR Table A-2 to Subpart A of... - Units of Measure Conversions
Code of Federal Regulations, 2014 CFR
2014-07-01
... Meters (m) Feet (ft) 3.28084 Miles (mi) Kilometers (km) 1.60934 Kilometers (km) Miles (mi) 0.62137 Square feet (ft2) Acres 2.29568 × 10−5 Square meters (m2) Acres 2.47105 × 10−4 Square miles (mi2) Square... Mercury (in Hg) 2.95334 × 10−4 Inches of Mercury (inHg) Pounds per square inch (psi) 0.49110 Pounds per...
40 CFR Table A-2 to Subpart A of... - Units of Measure Conversions
Code of Federal Regulations, 2010 CFR
2010-07-01
... Meters (m) Feet (ft) 3.28084 Miles (mi) Kilometers (km) 1.60934 Kilometers (km) Miles (mi) 0.62137 Square feet (ft2) Acres 2.29568 × 10−5 Square meters (m2) Acres 2.47105 × 10−4 Square miles (mi2) Square... Mercury (in Hg) 2.95334 × 10−4 Inches of Mercury (inHg) Pounds per square inch (psi) 0.49110 Pounds per...
40 CFR Table A-2 to Subpart A of... - Units of Measure Conversions
Code of Federal Regulations, 2011 CFR
2011-07-01
... Meters (m) Feet (ft) 3.28084 Miles (mi) Kilometers (km) 1.60934 Kilometers (km) Miles (mi) 0.62137 Square feet (ft2) Acres 2.29568 × 10−5 Square meters (m2) Acres 2.47105 × 10−4 Square miles (mi2) Square... Mercury (in Hg) 2.95334 × 10−4 Inches of Mercury (inHg) Pounds per square inch (psi) 0.49110 Pounds per...
40 CFR Table A-2 to Subpart A of... - Units of Measure Conversions
Code of Federal Regulations, 2012 CFR
2012-07-01
... Meters (m) Feet (ft) 3.28084 Miles (mi) Kilometers (km) 1.60934 Kilometers (km) Miles (mi) 0.62137 Square feet (ft2) Acres 2.29568 × 10−5 Square meters (m2) Acres 2.47105 × 10−4 Square miles (mi2) Square... Mercury (in Hg) 2.95334 × 10−4 Inches of Mercury (inHg) Pounds per square inch (psi) 0.49110 Pounds per...
40 CFR Table A-2 to Subpart A of... - Units of Measure Conversions
Code of Federal Regulations, 2013 CFR
2013-07-01
... Meters (m) Feet (ft) 3.28084 Miles (mi) Kilometers (km) 1.60934 Kilometers (km) Miles (mi) 0.62137 Square feet (ft2) Acres 2.29568 × 10−5 Square meters (m2) Acres 2.47105 × 10−4 Square miles (mi2) Square... Mercury (in Hg) 2.95334 × 10−4 Inches of Mercury (inHg) Pounds per square inch (psi) 0.49110 Pounds per...
16 CFR 500.12 - Measurement of commodities by length and width, how expressed.
Code of Federal Regulations, 2013 CFR
2013-01-01
... square foot (929 cm2) be expressed in terms of length and width in linear measure. The customary inch... of 1 square foot (929 cm2) or more, but less than 4 square feet (37.1 dm2), be expressed in terms of... in square inches with length and width expressed in the largest whole unit (yard or foot) with any...
16 CFR 500.12 - Measurement of commodities by length and width, how expressed.
Code of Federal Regulations, 2011 CFR
2011-01-01
... square foot (929 cm2) be expressed in terms of length and width in linear measure. The customary inch... of 1 square foot (929 cm2) or more, but less than 4 square feet (37.1 dm2), be expressed in terms of... in square inches with length and width expressed in the largest whole unit (yard or foot) with any...
16 CFR 500.12 - Measurement of commodities by length and width, how expressed.
Code of Federal Regulations, 2014 CFR
2014-01-01
... square foot (929 cm2) be expressed in terms of length and width in linear measure. The customary inch... of 1 square foot (929 cm2) or more, but less than 4 square feet (37.1 dm2), be expressed in terms of... in square inches with length and width expressed in the largest whole unit (yard or foot) with any...
16 CFR 500.12 - Measurement of commodities by length and width, how expressed.
Code of Federal Regulations, 2012 CFR
2012-01-01
... square foot (929 cm2) be expressed in terms of length and width in linear measure. The customary inch... of 1 square foot (929 cm2) or more, but less than 4 square feet (37.1 dm2), be expressed in terms of... in square inches with length and width expressed in the largest whole unit (yard or foot) with any...
Minor floods of 1938 in the North Atlantic States
,
1947-01-01
Five noteworthy floods occurred during 1938 in the North Atlantic States. The first flood was in January, the others were in June, July, August, and September. The floods of January, June, and August were relatively local events in Connecticut, New Jersey, and New York, respectively. The floods of July and September were widespread, reaching from New Jersey and New York to New Hampshire in generally coincident locations. The flood of September, the most severe, is described in appropriate detail in Water-Supply Paper 867; the others in this volume are in separate sections arranged chronologically. Extraordinary floods in Connecticut during January 1938 resulted from a critical combination of warm rainfall and virtual overnight melting of the accumulated snowfall of winter. Seven small streams in central and western Connecticut rose to levels on January 25 higher than those reached during the great floods of March 1936. Crest discharge of these streams approximated 100 second-feet per square mile. Ice cover was loosened and sent downstream in recurrent jams. In general, the larger rivers did not attain extraordinary stages. The Connecticut River at Hartford peaked at a stage 3.6 feet above ordinary flood level. Direct damage by the flood was relatively small. Snow cover on January 20, at the beginning of the rains, varied from 0.25 inch along the coast to 2.75 inches water equivalent in the northern part of the State. Precipitation between January 24 and 26 exceeded 2.75 inches in only three small areas. Total supply as water in snow and precipitation did not exceed 4.8 inches over any tributary area. Maximum measured flood run-off was 2.7 inches. The flood of June 1938 in New Jersey was the immediate result of a 30-hour rainstorm on June 26-27 that centered along a line extending from Odessa, Del., to Milton, N. J. Storm rainfall exceeded 5 inches over a total area of 2,900 square miles. River stages in the central parts of the storm area rose to levels that approached and on a few rivers exceeded previous maxima of record. Damage was extensive throughout the storm area, especially in Burlington, N. J., where Sylvan Lake Dam failed. The highest rate of flow per unit of area measured was 88 second-feet per square mile. However, all peak discharges were exceeded during the later floods of 1938 or by the flood of September 1, 1940, which produced discharges over 1,000 second-feet per square mile in southern New Jersey. The maximum volume of direct runoff during the flood, expressed in mean depth in inches on the drainage area, was 2.1 inches. From July 17 to 25, 1938, there was an irregular series of rainstorms over the eastern seaboard that brought more than 10 inches of rain over an area of 2,000 square miles and more than 6 inches over 23,000 square miles. Nearly 14 inches of rain fell at Long Branch, N. J. Extraordinary floods occurred mainly in the smaller tributary streams. Damage to highways, homes, factories, and crops, particularly the tobacco co-op in Connecticut, was extensive. Crest discharges at 12 gaging stations exceeded those previously observed. Maximum rates of discharge varied from 601 second-feet per square mile for an area of 2.91 square miles in New Jersey to 35 second-feet per square mile for an area of 711 square miles in Connecticut. Antecedent soil moisture prior to the storm was probably normal or a little above. The maximum volume of direct runoff was 4.75 inches in Massachusetts, 5.6 inches in eastern Connecticut, 6.75 inches in the Catskill Mountain region of New York, and 4.95 inches in the Raritan River Basin of New Jersey. Infiltration indices from 0.09 .to 0.21 inch per hour were computed, such rates being within the range defined for basins in the same areas during the floods of September 1938. The flood of August 6-11, 1938, in the Catskill Mountain region of New York resulted from heavy rains with a maximum of 8 inches at two centers. Rainfall exceeded 3 inches over more than 3,000
33 CFR 118.100 - Retroreflective panels on bridge piers.
Code of Federal Regulations, 2011 CFR
2011-07-01
... six inches square. If the visibility required is more than one-half mile, the panels must be at least 12 inches square. (c) To mark bridge piers or channel sides on bridges not required to have bridge lighting. Lateral significant red triangles and green square retroreflective panels shall be used. The...
Code of Federal Regulations, 2012 CFR
2012-10-01
...) Leakage from the main air reservoir and related piping may not exceed an average of 3 pounds per square.... (b) Brake pipe leakage may not exceed 5 pounds per square inch per minute. (c) With a full service... pneumatically operated controls may not exceed an average of 3 pounds per square inch per minute for 3 minutes...
Code of Federal Regulations, 2014 CFR
2014-10-01
...) Leakage from the main air reservoir and related piping may not exceed an average of 3 pounds per square.... (b) Brake pipe leakage may not exceed 5 pounds per square inch per minute. (c) With a full service... pneumatically operated controls may not exceed an average of 3 pounds per square inch per minute for 3 minutes...
Code of Federal Regulations, 2013 CFR
2013-10-01
...) Leakage from the main air reservoir and related piping may not exceed an average of 3 pounds per square.... (b) Brake pipe leakage may not exceed 5 pounds per square inch per minute. (c) With a full service... pneumatically operated controls may not exceed an average of 3 pounds per square inch per minute for 3 minutes...
Code of Federal Regulations, 2010 CFR
2010-10-01
...) Leakage from the main air reservoir and related piping may not exceed an average of 3 pounds per square.... (b) Brake pipe leakage may not exceed 5 pounds per square inch per minute. (c) With a full service... pneumatically operated controls may not exceed an average of 3 pounds per square inch per minute for 3 minutes...
49 CFR 229.49 - Main reservoir system.
Code of Federal Regulations, 2014 CFR
2014-10-01
... least one safety valve that shall prevent an accumulation of pressure of more than 15 pounds per square... or unloads and loads the air compressor within 5 pounds per square inch above or below the maximum... pressure is not less than 15 pounds per square inch above the maximum brake pipe pressure fixed by the...
Code of Federal Regulations, 2011 CFR
2011-10-01
...) Leakage from the main air reservoir and related piping may not exceed an average of 3 pounds per square.... (b) Brake pipe leakage may not exceed 5 pounds per square inch per minute. (c) With a full service... pneumatically operated controls may not exceed an average of 3 pounds per square inch per minute for 3 minutes...
49 CFR 229.49 - Main reservoir system.
Code of Federal Regulations, 2010 CFR
2010-10-01
... least one safety valve that shall prevent an accumulation of pressure of more than 15 pounds per square... or unloads and loads the air compressor within 5 pounds per square inch above or below the maximum... pressure is not less than 15 pounds per square inch above the maximum brake pipe pressure fixed by the...
33 CFR 118.100 - Retroreflective panels on bridge piers.
Code of Federal Regulations, 2014 CFR
2014-07-01
... six inches square. If the visibility required is more than one-half mile, the panels must be at least 12 inches square. (c) To mark bridge piers or channel sides on bridges not required to have bridge lighting. Lateral significant red triangles and green square retroreflective panels shall be used. The...
33 CFR 118.100 - Retroreflective panels on bridge piers.
Code of Federal Regulations, 2010 CFR
2010-07-01
... six inches square. If the visibility required is more than one-half mile, the panels must be at least 12 inches square. (c) To mark bridge piers or channel sides on bridges not required to have bridge lighting. Lateral significant red triangles and green square retroreflective panels shall be used. The...
33 CFR 118.100 - Retroreflective panels on bridge piers.
Code of Federal Regulations, 2012 CFR
2012-07-01
... six inches square. If the visibility required is more than one-half mile, the panels must be at least 12 inches square. (c) To mark bridge piers or channel sides on bridges not required to have bridge lighting. Lateral significant red triangles and green square retroreflective panels shall be used. The...
33 CFR 118.100 - Retroreflective panels on bridge piers.
Code of Federal Regulations, 2013 CFR
2013-07-01
... six inches square. If the visibility required is more than one-half mile, the panels must be at least 12 inches square. (c) To mark bridge piers or channel sides on bridges not required to have bridge lighting. Lateral significant red triangles and green square retroreflective panels shall be used. The...
A polytetrafluorethylene insulated cable for high temperature oxygen aerospace applications
NASA Technical Reports Server (NTRS)
Sheppard, A. T.; Webber, R. G.
1983-01-01
For electrical cables to function and survive in the severe high temperature oxygen environment that will be experienced in the external tanks of the space shuttle, extreme cleanliness and material purity is required. A flexible light weight cable has been developed for use in pure oxygen at worst case temperatures of -190 to +260 degrees Centigrade and pressures as high as 44 pounds per square inch absolute. A comprehensive series of tests were performed on cables manufactured to the best commercial practices in order to establish the basic guidelines for control of build configuration as well as each material used in construction of the cable.
Theoretical Performance of Hydrogen-Oxygen Rocket Thrust Chambers
NASA Technical Reports Server (NTRS)
Sievers, Gilbert K.; Tomazic, William A.; Kinney, George R.
1961-01-01
Data are presented for liquid-hydrogen-liquid-oxygen thrust chambers at chamber pressures from 15 to 1200 pounds per square inch absolute, area ratios to approximately 300, and percent fuel from about 8 to 34 for both equilibrium and frozen composition during expansion. Specific impulse in vacuum, specific impulse, combustion-chamber temperature, nozzle-exit temperature, characteristic velocity, and the ratio of chamber-to-nozzle-exit pressure are included. The data are presented in convenient graphical forms to allow quick calculation of theoretical nozzle performance with over- or underexpansion, flow separation, and introduction of the propellants at various initial conditions or heat loss from the combustion chamber.
NASA Technical Reports Server (NTRS)
Gordon, Sanford; Kastner, Michael E
1958-01-01
Theoretical rocket performance for frozen composition during expansion was calculated for liquid methane with several fluorine-oxygen mixtures for a range of pressure ratios and oxidant-fuel ratios. The parameters included are specific impulse, combustion-chamber temperature, nozzle-exit temperature molecular weight, characteristic velocity, coefficient of thrust, ratio of nozzle-exit area to throat area, specific heat at constant pressure, isentropic exponent, viscosity, and thermal conductivity. The maximum calculated value of specific impulse for a chamber pressure of 600 pounds per square inch absolute (40.827atm) and an exit pressure of 1 atmosphere is 315.3 for 79.67 percent fluorine in the oxidant.
A polytetrafluorethylene insulated cable for high temperature oxygen aerospace applications
NASA Astrophysics Data System (ADS)
Sheppard, A. T.; Webber, R. G.
For electrical cables to function and survive in the severe high temperature oxygen environment that will be experienced in the external tanks of the space shuttle, extreme cleanliness and material purity is required. A flexible light weight cable has been developed for use in pure oxygen at worst case temperatures of -190 to +260 degrees Centigrade and pressures as high as 44 pounds per square inch absolute. A comprehensive series of tests were performed on cables manufactured to the best commercial practices in order to establish the basic guidelines for control of build configuration as well as each material used in construction of the cable.
NASA Technical Reports Server (NTRS)
Miller, Riley O.; Brown, Dwight D.
1959-01-01
An experimental study shows that 2 percent by weight ozone in oxygen has little effect on overall reactivity for a range of oxidant-fuel weight ratios from 1 to 6. This conclusion is based on characteristic-velocity measurements in 200-pound-thrust chambers at a pressure of 300 pounds per square inch absolute with low-efficiency injectors. The presence of 9 percent ozone in oxygen also did not affect performance in an efficient chamber. Explosions were encountered when equipment or procedure permitted ozone to concentrate locally. These experiments indicate that even small amounts of ozone in oxygen can cause operational problems.
HYDROSTATIC PRESSURE AND TEMPERATURE IN RELATION TO STIMULATION AND CYCLOSIS IN NITELLA FLEXILIS
Harvey, E. Newton
1942-01-01
Nitella flexilis cells are not stimulated to "shock stoppage" of cyclosis by suddenly evacuating the air over the water or on sudden readmission of air, or on suddenly striking a piston in the water-filled chamber in which they are kept with a ball whose energy is 7.6 joules, provided the Nitella cell is not moved by currents against the side of the chamber. Sudden increases in hydrostatic pressure from zero to 1000 lbs. or 0 to 5000 lbs. per square inch or 5000 to 9000 lbs. per square inch usually do not stimulate to "shock stoppage" of cyclosis, but some cells are stimulated. Sudden decreases of pressure are more likely to stimulate, again with variation depending on the cell. In the absence of stimulation, the cyclosis velocity at 23°C. slows as the pressure is increased in steps of 1000 lbs. per square inch. In some cells a regular slowing is observed, in others there is little slowing until 4000 to 6000 lbs. per square inch, when a rapid slowing appears, with only 50 per cent to 30 per cent of the original velocity at 9000 lbs. per square inch. The cyclosis does not completely stop at 10000 lbs. per square inch. The pressure effect is reversible unless the cells have been kept too long at the high pressure. At low temperatures (10°C.) and at temperatures near and above (32°–38°C.) the optimum temperature for maximum cyclosis (35–36°C.) pressures of 3000 to 6000 lbs. per square inch cause only further slowing of cyclosis, with no reversal of the temperature effect, such as has been observed in pressure-temperature studies on the luminescence of luminous bacteria. Sudden increase in temperature may cause shock stoppage of cyclosis as well as sudden decrease in temperature. PMID:19873318
21 CFR 178.3290 - Chromic chloride complexes.
Code of Federal Regulations, 2014 CFR
2014-04-01
... square inch of closure area. (b) The packaging container which has its closure area treated with the release agent shall have a capacity of not less than 120 grams of food per square inch of such treated...
Wright St Univ Participation in AFRL University Engineering Design Challenge
2014-12-23
18 Figure 9: Loading results from 10 min. heat treatment cure on 1 square inch Kevlar Patch, air cool, and concrete...loading and Average for Three Trials of 10 min heat treatment cure, 1 square inch Kevlar Patch, air cool, and concrete...19 Figure 11: Loading results from 10 min. heat treatment cure on 1 square
49 CFR 230.25 - Maximum allowable stress on stays and braces.
Code of Federal Regulations, 2012 CFR
2012-10-01
... maximum allowable stress per square inch of net cross sectional area on fire box and combustion chamber stays shall be 7,500 psi. The maximum allowable stress per square inch of net cross sectional area on...
49 CFR 230.25 - Maximum allowable stress on stays and braces.
Code of Federal Regulations, 2014 CFR
2014-10-01
... maximum allowable stress per square inch of net cross sectional area on fire box and combustion chamber stays shall be 7,500 psi. The maximum allowable stress per square inch of net cross sectional area on...
49 CFR 230.25 - Maximum allowable stress on stays and braces.
Code of Federal Regulations, 2011 CFR
2011-10-01
... maximum allowable stress per square inch of net cross sectional area on fire box and combustion chamber stays shall be 7,500 psi. The maximum allowable stress per square inch of net cross sectional area on...
49 CFR 230.25 - Maximum allowable stress on stays and braces.
Code of Federal Regulations, 2013 CFR
2013-10-01
... maximum allowable stress per square inch of net cross sectional area on fire box and combustion chamber stays shall be 7,500 psi. The maximum allowable stress per square inch of net cross sectional area on...
2013-09-01
Factors Multiply By To Obtain cubic inches 1.6387064 E -05 cubic meters inches 0.0254 meters pounds (force) 4.448222 newtons pounds (force) per...0.45359237 kilograms pounds (mass) per cubic foot 16.01846 kilograms per cubic meter pounds (mass) per cubic inch 2.757990 E +04 kilograms per cubic...14.59390 kilograms square inches 6.4516 E -04 square meters ERDC/ITL TR-13-4 1 1 Introduction 1.1 Bio–inspiration Nature has evolved from a
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.
30 CFR 75.1719-4 - Mining machines, cap lamps; requirements.
Code of Federal Regulations, 2011 CFR
2011-07-01
... or reflecting tape shall have an area of not less than 10 square inches. (c) Each person who goes... of 6 square inches of reflecting tape or equivalent paint or material on each side and back. [41 FR...
30 CFR 75.1719-4 - Mining machines, cap lamps; requirements.
Code of Federal Regulations, 2010 CFR
2010-07-01
... or reflecting tape shall have an area of not less than 10 square inches. (c) Each person who goes... of 6 square inches of reflecting tape or equivalent paint or material on each side and back. [41 FR...
30 CFR 75.1719-4 - Mining machines, cap lamps; requirements.
Code of Federal Regulations, 2013 CFR
2013-07-01
... or reflecting tape shall have an area of not less than 10 square inches. (c) Each person who goes... of 6 square inches of reflecting tape or equivalent paint or material on each side and back. [41 FR...
Effect of Water Immersion on Fiber/Matrix Adhesion
1993-01-01
ABBREVIATIONS 0C Degrees Centigrade KSI Thousand Pounds Per Square Inch MSI Million Pounds Per Square Inch OCF Owens Corning Fiberglas PEEK...A209 Dr. David Hartman Gaithersburg, MD 20899 Owens - Corning Fiberglas Corp. Technical Center Dr. Forrest Sloan 2790 Columbus Road, Rt. 16 Allied
Theoretical performance of liquid hydrogen and liquid fluorine as a rocket propellant
NASA Technical Reports Server (NTRS)
Gordon, Sanford; Huff, Vearl N
1953-01-01
Theoretical values of performance parameters for liquid hydrogen and liquid fluorine as a rocket propellant were calculated on the assumption of equilibrium composition during the expansion process for a wide range of fuel-oxidant and expansion ratios. The parameters included were specific impulse, combustion-chamber temperature, nozzle-exit temperature, equilibrium composition, mean molecular weight, characteristic velocity, coefficient of thrust, ration of nozzle-exit area to throat area, specific heat at constant pressure, coefficient of viscosity, and coefficient of thermal conductivity. The maximum value of specific impulse was 364.6 pound-seconds per pound for a chamber pressure of 300 pounds per square inch absolute (20.41 atm) and an exit pressure of 1 atmosphere.
Theoretical performance of liquid ammonia and liquid fluorine as a rocket propellant
NASA Technical Reports Server (NTRS)
Gordon, Sanford; Huff, Vearl N
1953-01-01
Theoretical values of performance parameters for liquid ammonia and liquid fluorine as a rocket propellant were calculated on the assumption of equilibrium composition during the expansion process for a wide range of fuel-oxidant and expansion ratios. The parameters included were specific impulse, combustion chamber temperature, nozzle-exit temperature, equilibrium composition, mean molecular weight, characteristic velocity, coefficient of thrust, ratio of nozzle-exit area to throat area, specific heat at constant pressure, coefficient of viscosity, and coefficient of thermal conductivity. The maximum value of specific impulse was 311.5 pound-seconds per pound for a chamber pressure of 300 pounds per square inch absolute (20.41 atm) and an exit pressure of 1 atmosphere.
Breeding, Seth D.
1948-01-01
Floods occurred in Texas during, June, July, and November 1940 that exceeded known stages on many small streams and at a few places on the larger streams. Stages at several stream-gaging stations exceeded the maximum known at those places since the collection of daily records began. A storm, haying its axis generally on a north-south line from Cameron to Victoria and extending across the Brazos, Colorado, Lavaca, and Guadalupe River Basins, caused heavy rainfall over a large part of south-central Texas. The maximum recorded rain of 22.7 inches for the 2-day period June 29-30 occurred at Engle. Of this amount, 17.5 inches fell in the 12-hour period between 8 p.m. June 29, and 8 a.m. June 30. Light rains fell at a number of places on June 28, and additional light rains fell at many places within the area from July 1 to 4. During the period June 28 to July 4 more than 20 inches of rain fell over an area of 300 square miles, more than 15 inches over 1,920 square miles, and more than 10 inches over 5,100 square miles. The average annual rainfall for the area experiencing the heaviest rainfall during this storm is about 35 inches. Farming is largely confined to the fertile flood plains in much of the area subjected to the record-breaking floods in June and July. Therefore these floods, coming at the height of the growing season, caused severe losses to crops. Much damage was done also to highways and railways. The city of Hallettsville suffered the greatest damage of any urban area. The Lavaca River at that place reached a stage 8 feet higher than ever known before, drowned several people, destroyed many homes, and submerged almost the entire business district. The maximum discharge there was 93,100 second-feet from a drainage area of 101 square miles. Dry Creek near Smithville produced a maximum discharge of 1,879 second-feet from an area of 1.48 square miles and a runoff of 11.3 inches in a 2-day period from a rainfall of 19.5 inches. The area in the Colorado River Basin between Smithville and La Grange, amounting to 550 square miles, had an average rainfall of 19.3 inches, of which 11.5 inches appeared as runoff. The maximum discharge at La Grange was 182,000 second-feet, with much the greater part coming from below Smithville. This is probably a record-breaking flood for the area between Smithville and La Grange, but stages as much as 16 feet higher have occurred at La Grange. Heavy rainfall over the east half of Texas November 21-26 caused large floods in all streams in Texas east of the Guadalupe River. The maximum recorded rainfall for the 2-day period November 24-25 was 20.46 inches at Hempstead, of which 16.00 inches fell in 24 hours or less. The storm occurred during the period November 20-26, with the greater part of the rain falling November 23-25. During the period November 20-26, rainfall in Texas amounted to more than 15 inches over an area of 3,380 square miles, and 'to more than 10 inches over an area of 17,570 square miles. The average annual rainfall for the area in Texas experiencing more than 10 inches of rain during this storm ranges from 501 inches on the east border of the State to 35 inches near the west edge of the area. The study of this storm for the purposes of this report is limited to the San Jacinto River Basin, which had an average rainfall of 13.6 inches. This basin has an area of 2,791 square miles above the gaging station near Huffman and is typical in topographic and hydrologic features of much of eastern Texas. The stage reached at the gage near Huffman was about 1 foot higher than known before, the maximum discharge was 253,000 second-feet, and the runoff from the storm amounted to 8.8 inches. The November flood came after crops had been harvested, and its damage was mainly the destruction of highways and railways and the drowning of livestock. The storage reservoirs on the Colorado River located well upstream from the storm areas herein studied had very little effect on
40 CFR 49.128 - Rule for limiting particulate matter emissions from wood products industry sources.
Code of Federal Regulations, 2014 CFR
2014-07-01
... veneer dryers must not exceed 0.3 pounds per 1000 square feet of veneer dried (3/8 inch basis), one-hour average. (ii) PM10 emissions from steam heated veneer dryers must not exceed 0.3 pounds per 1000 square... dryers must not exceed a total of 0.3 pounds per 1000 square feet of veneer dried (3/8 inch basis) and 0...
46 CFR 32.60-35 - Tank vessels carrying Grade A liquid cargo-TB/ALL.
Code of Federal Regulations, 2013 CFR
2013-10-01
... Reid vapor pressure in excess of 25 pounds per square inch shall be transported in cargo tanks which... excess of 25 pounds per square inch shall be of a Type III barge hull as defined in § 32.63-5(b)(3...
46 CFR 32.60-35 - Tank vessels carrying Grade A liquid cargo-TB/ALL.
Code of Federal Regulations, 2010 CFR
2010-10-01
... Reid vapor pressure in excess of 25 pounds per square inch shall be transported in cargo tanks which... excess of 25 pounds per square inch shall be of a Type III barge hull as defined in § 32.63-5(b)(3...
46 CFR 32.60-35 - Tank vessels carrying Grade A liquid cargo-TB/ALL.
Code of Federal Regulations, 2014 CFR
2014-10-01
... Reid vapor pressure in excess of 25 pounds per square inch shall be transported in cargo tanks which... excess of 25 pounds per square inch shall be of a Type III barge hull as defined in § 32.63-5(b)(3...
46 CFR 32.60-35 - Tank vessels carrying Grade A liquid cargo-TB/ALL.
Code of Federal Regulations, 2011 CFR
2011-10-01
... Reid vapor pressure in excess of 25 pounds per square inch shall be transported in cargo tanks which... excess of 25 pounds per square inch shall be of a Type III barge hull as defined in § 32.63-5(b)(3...
46 CFR 32.60-35 - Tank vessels carrying Grade A liquid cargo-TB/ALL.
Code of Federal Regulations, 2012 CFR
2012-10-01
... Reid vapor pressure in excess of 25 pounds per square inch shall be transported in cargo tanks which... excess of 25 pounds per square inch shall be of a Type III barge hull as defined in § 32.63-5(b)(3...
DOE Office of Scientific and Technical Information (OSTI.GOV)
Murton, Mark; Bouchier, Francis A.; vanDongen, Dale T.
2013-08-01
Although technological advances provide new capabilities to increase the robustness of security systems, they also potentially introduce new vulnerabilities. New capability sometimes requires new performance requirements. This paper outlines an approach to establishing a key performance requirement for an emerging intrusion detection sensor: the sensored net. Throughout the security industry, the commonly adopted standard for maximum opening size through barriers is a requirement based on square inchestypically 96 square inches. Unlike standard rigid opening, the dimensions of a flexible aperture are not fixed, but variable and conformable. It is demonstrably simple for a human intruder to move through a 96-square-inchmore » opening that is conformable to the human body. The longstanding 96-square-inch requirement itself, though firmly embedded in policy and best practice, lacks a documented empirical basis. This analysis concluded that the traditional 96-square-inch standard for openings is insufficient for flexible openings that are conformable to the human body. Instead, a circumference standard is recommended for these newer types of sensored barriers. The recommended maximum circumference for a flexible opening should be no more than 26 inches, as measured on the inside of the netting material.« less
Elevated Temperature Properties of Titanium Carbide Base Ceramals Containing Nickel or Iron
NASA Technical Reports Server (NTRS)
Cooper, A L; Colteryahn, L E
1951-01-01
Elevated-temperature properties of titanium carbide base ceramals containing nickel or iron were determined in oxidation, modulus of rupture, tensile strength, and thermal-shock resistance. These materials followed the general growth law and exhibited two stages in oxidation. The following tensile strengths were found at 2000 degrees F: 13.3 weight percent nickel, 16, 150 pounds per square inch; 11.8 weight percent iron, 12,500 pounds per square inch; unalloyed titanium carbide, 16,450 pounds per square inch. Nickel or iron additions to titanium carbide improved the thermal-shock resistance, nickel more. The path of fracture in tensile and thermal-shock specimens was found to progress approximately 50 percent intergranularly and 50 percent transgranularly.
16 CFR 500.8 - Units of weight or mass and measure.
Code of Federal Regulations, 2011 CFR
2011-01-01
... shall be in terms of both square yards, square feet, and square inches and SI metric square meters, square decimeters, square centimeters, or square millimeters. (e) Statements of dry measure shall be in...
16 CFR 500.8 - Units of weight or mass and measure.
Code of Federal Regulations, 2010 CFR
2010-01-01
... shall be in terms of both square yards, square feet, and square inches and SI metric square meters, square decimeters, square centimeters, or square millimeters. (e) Statements of dry measure shall be in...
16 CFR 500.8 - Units of weight or mass and measure.
Code of Federal Regulations, 2013 CFR
2013-01-01
... shall be in terms of both square yards, square feet, and square inches and SI metric square meters, square decimeters, square centimeters, or square millimeters. (e) Statements of dry measure shall be in...
16 CFR 500.8 - Units of weight or mass and measure.
Code of Federal Regulations, 2014 CFR
2014-01-01
... be in terms of both square yards, square feet, and square inches and SI metric square meters, square decimeters, square centimeters, or square millimeters. (e) Statements of dry measure shall be in terms of...
16 CFR 500.8 - Units of weight or mass and measure.
Code of Federal Regulations, 2012 CFR
2012-01-01
... shall be in terms of both square yards, square feet, and square inches and SI metric square meters, square decimeters, square centimeters, or square millimeters. (e) Statements of dry measure shall be in...
NASA Technical Reports Server (NTRS)
Rothenberg, Edward A; Ordin, Paul M
1954-01-01
The performance of jet fuel with an oxidant mixture containing 70 percent liquid fluorine and 30 percent liquid oxygen by weight was investigated in a 500-pound-thrust engine operating at a chamber pressure of 300 pounds per square inch absolute. A one-oxidant-on-one-fuel skewed-hole impinging-jet injector was evaluated in a chamber of characteristic length equal to 50 inches. A maximum experimental specific impulse of 268 pound-seconds per pound was obtained at 25 percent fuel, which corresponds to 96 percent of the maximum theoretical specific impulse based on frozen composition expansion. The maximum characteristic velocity obtained was 6050 feet per second at 23 percent fuel, or 94 percent of the theoretical maximum. The average thrust coefficient was 1.38 for the 500-pound thrust combustion-chamber nozzle used, which was 99 percent of the theoretical (frozen) maximum. Mixtures of fluorine and oxygen were found to be self-igniting with jet fuel with fluorine concentrations as low as 4 percent, when low starting propellant flow rated were used.
1998-08-10
In the Tile Fabrication Shop, Tony Rollins, with United Space Alliance, holds down a curtain while making a test sample of tile on a block 5-axis computerized numerical control milling machine. About 70 percent of a Space Shuttle orbiter’s external surface is shielded from heat by a network of more than 24,000 tiles formed from a silica fiber compound. They are known as High-Temperature Reusable Surface Insulation (HRSI) tiles and Low-Temperature Reusable Surface Insulation (LRSI) tiles. Most HRSI tiles are 6 inches square, but may be as large as 12 inches in some areas, and 1 to 5 inches thick. LRSI tiles are generally 8 inches square, ranging from 0.2to 1-inch thick. More advanced materials such as Flexible Insulation Blankets have replaced tiles on some upper surfaces of the orbiter
Code of Federal Regulations, 2012 CFR
2012-07-01
...) Bearing plates used directly against the mine roof shall be at least 6 inches square or the equivalent... or the equivalent may be used. (3) Bearing plates used with wood or metal materials shall be at least 4 inches square or the equivalent. (4) Wooden materials that are used between a bearing plate and...
Code of Federal Regulations, 2010 CFR
2010-07-01
...) Bearing plates used directly against the mine roof shall be at least 6 inches square or the equivalent... or the equivalent may be used. (3) Bearing plates used with wood or metal materials shall be at least 4 inches square or the equivalent. (4) Wooden materials that are used between a bearing plate and...
Code of Federal Regulations, 2011 CFR
2011-07-01
...) Bearing plates used directly against the mine roof shall be at least 6 inches square or the equivalent... or the equivalent may be used. (3) Bearing plates used with wood or metal materials shall be at least 4 inches square or the equivalent. (4) Wooden materials that are used between a bearing plate and...
Code of Federal Regulations, 2013 CFR
2013-07-01
...) Bearing plates used directly against the mine roof shall be at least 6 inches square or the equivalent... or the equivalent may be used. (3) Bearing plates used with wood or metal materials shall be at least 4 inches square or the equivalent. (4) Wooden materials that are used between a bearing plate and...
Tony Rollins fashions a new tile for the Space Shuttle orbiter
NASA Technical Reports Server (NTRS)
1998-01-01
In the Tile Fabrication Shop, Tony Rollins, with United Space Alliance, holds down a curtain while making a test sample of tile on a block 5-axis computerized numerical control milling machine. About 70 percent of a Space Shuttle orbiter's external surface is shielded from heat by a network of more than 24,000 tiles formed from a silica fiber compound. They are known as High-Temperature Reusable Surface Insulation (HRSI) tiles and Low-Temperature Reusable Surface Insulation (LRSI) tiles. Most HRSI tiles are 6 inches square, but may be as large as 12 inches in some areas, and 1 to 5 inches thick. LRSI tiles are generally 8 inches square, ranging from 0.2- to 1-inch thick. More advanced materials such as Flexible Insulation Blankets have replaced tiles on some upper surfaces of the orbiter.
46 CFR 190.20-20 - Sleeping accommodations.
Code of Federal Regulations, 2011 CFR
2011-10-01
... persons. (c) Each room must be of such size that there are at least 2.78 square meters (30 square feet) of deck area and a volume of at least 5.8 cubic meters (210 cubic feet) for each person accommodated. The... size of a berth must not be less than 68 centimeters (27 inches) wide by 190 centimeters (75 inches...
77 FR 59673 - Petitions for Modification of Application of Existing Mandatory Safety Standards
Federal Register 2010, 2011, 2012, 2013, 2014
2012-09-28
... will examine valves and nozzles for damage malfunction and close the door fully before opening the air... failure pressure of 1,300 pounds per square inch, capped at the base, and actuated by an electrically controlled ball valve at the top. 6. Air nozzles must not exceed 30 pounds per square inch gauge. 7. The...
Concept Demonstration of Dopant Selective Reactive Etching (DSRIE) in Silicon Carbide
NASA Technical Reports Server (NTRS)
Okojie, Robert S.
2015-01-01
Accurate quantification of combustor pressure dynamics for the primary purpose of experimental validation of computational fluid dynamics (CFD) codes requires the use of robust, reliable and sensitive pressure sensors that can resolve sub--pound-per-square-inch pressure levels in high temperature environments (i.e., combustor). The state of the art microfabricated piezoresistive silicon carbide (SiC) pressure sensors that we have developed are capable of operating reliably at 600 degrees Centigrade. This technology was used in support of the ARMD ISRP-ERA (NASA's Aeronautics Research Mission Directorate, Integrated System Research Project - Environmentally Responsible Aviation) program to quantify combustor thermoacoustic instabilities. The results showed that while the SiC pressure sensors survived the high temperature and measured instabilities, the diaphragm (force collector) was not thin enough to be sensitive in resolving sub-pound-per-square-inch pressures; 30 meters is the thinnest diaphragm achievable with conventional reactive ion etching (RIE) processes. Therefore, this precludes its use for sub-pound-per-square-inch pressure measurement with high fidelity. In order to effectively resolve sub-pound-per-square-inch pressures, a thinner more sensitive diaphragm (10 meters) is needed. To achieve this would require a new and innovative fabrication process technique.
50 CFR 648.84 - Gear-marking requirements and gear restrictions.
Code of Federal Regulations, 2014 CFR
2014-10-01
... extension of a rope separator trawl must be 6-inch (15.2-cm) diamond mesh or 6.5-inch (16.5-cm) square mesh, or any combination thereof. Mesh in the bottom belly of the net must be 13-inch (33-cm) diamond mesh...
50 CFR 648.84 - Gear-marking requirements and gear restrictions.
Code of Federal Regulations, 2013 CFR
2013-10-01
... extension of a rope separator trawl must be 6-inch (15.2-cm) diamond mesh or 6.5-inch (16.5-cm) square mesh, or any combination thereof. Mesh in the bottom belly of the net must be 13-inch (33-cm) diamond mesh...
Closure of logging wounds after 10 years
H. Clay Smith; Gary W. Miller; Thomas M. Schuler
1994-01-01
Closure of logging wounds on 96 sample trees was evaluated after 2, 5, and 10 years for Appalachian hardwood trees in north-central West Virginia. For yellow-poplar, northern red oak, black cherry, and white oak, many small wounds, 1 to 50 square inches in size, closed between 5 and 10 years after logging. For larger wounds, 50 to 200 square inches, it appears that...
Code of Federal Regulations, 2013 CFR
2013-10-01
... square. Square-fit taper: Nominally two (2) in twelve (12) inches (see Plate A). (vi) All chains shall be not less than nine-sixteenths (9/16) inch BBB coil chain. (vii) All handbrake rods shall be not less... coupler horn against the buffer block or end sill. (iii) Handbrake housing shall be securely fastened to...
49 CFR 231.1 - Box and other house cars built or placed in service before October 1, 1966.
Code of Federal Regulations, 2013 CFR
2013-10-01
... and passing through the inside face of knuckle when closed with coupler horn against the buffer block... brake-shaft step which will permit the brake chain to drop under the brake shaft shall not be used. U...-eighths of an inch square. Square-fit taper, nominally 2 in 12 inches. (See plate A.) (vi) Brake chain...
49 CFR 231.1 - Box and other house cars built or placed in service before October 1, 1966.
Code of Federal Regulations, 2010 CFR
2010-10-01
... and passing through the inside face of knuckle when closed with coupler horn against the buffer block... brake-shaft step which will permit the brake chain to drop under the brake shaft shall not be used. U...-eighths of an inch square. Square-fit taper, nominally 2 in 12 inches. (See plate A.) (vi) Brake chain...
Code of Federal Regulations, 2012 CFR
2012-10-01
... square. Square-fit taper: Nominally two (2) in twelve (12) inches (see Plate A). (vi) All chains shall be not less than nine-sixteenths (9/16) inch BBB coil chain. (vii) All handbrake rods shall be not less... coupler horn against the buffer block or end sill. (iii) Handbrake housing shall be securely fastened to...
49 CFR 231.1 - Box and other house cars built or placed in service before October 1, 1966.
Code of Federal Regulations, 2011 CFR
2011-10-01
... and passing through the inside face of knuckle when closed with coupler horn against the buffer block... brake-shaft step which will permit the brake chain to drop under the brake shaft shall not be used. U...-eighths of an inch square. Square-fit taper, nominally 2 in 12 inches. (See plate A.) (vi) Brake chain...
Code of Federal Regulations, 2014 CFR
2014-10-01
... square. Square-fit taper: Nominally two (2) in twelve (12) inches (see Plate A). (vi) All chains shall be not less than nine-sixteenths (9/16) inch BBB coil chain. (vii) All handbrake rods shall be not less... coupler horn against the buffer block or end sill. (iii) Handbrake housing shall be securely fastened to...
49 CFR 231.1 - Box and other house cars built or placed in service before October 1, 1966.
Code of Federal Regulations, 2012 CFR
2012-10-01
... and passing through the inside face of knuckle when closed with coupler horn against the buffer block... brake-shaft step which will permit the brake chain to drop under the brake shaft shall not be used. U...-eighths of an inch square. Square-fit taper, nominally 2 in 12 inches. (See plate A.) (vi) Brake chain...
Code of Federal Regulations, 2011 CFR
2011-10-01
... square. Square-fit taper: Nominally two (2) in twelve (12) inches (see Plate A). (vi) All chains shall be not less than nine-sixteenths (9/16) inch BBB coil chain. (vii) All handbrake rods shall be not less... coupler horn against the buffer block or end sill. (iii) Handbrake housing shall be securely fastened to...
Code of Federal Regulations, 2010 CFR
2010-10-01
... square. Square-fit taper: Nominally two (2) in twelve (12) inches (see Plate A). (vi) All chains shall be not less than nine-sixteenths (9/16) inch BBB coil chain. (vii) All handbrake rods shall be not less... coupler horn against the buffer block or end sill. (iii) Handbrake housing shall be securely fastened to...
49 CFR 231.1 - Box and other house cars built or placed in service before October 1, 1966.
Code of Federal Regulations, 2014 CFR
2014-10-01
... and passing through the inside face of knuckle when closed with coupler horn against the buffer block... brake-shaft step which will permit the brake chain to drop under the brake shaft shall not be used. U...-eighths of an inch square. Square-fit taper, nominally 2 in 12 inches. (See plate A.) (vi) Brake chain...
50 CFR 648.91 - Monkfish regulated mesh areas and restrictions on gear and methods of fishing.
Code of Federal Regulations, 2014 CFR
2014-10-01
...-inch (25.4-cm) square or 12-inch (30.5-cm) diamond mesh throughout the codend for at least 45... gillnets used by a vessel fishing under a monkfish DAS is 10-inch (25.4-cm) diamond mesh, unless otherwise...
50 CFR 648.91 - Monkfish regulated mesh areas and restrictions on gear and methods of fishing.
Code of Federal Regulations, 2012 CFR
2012-10-01
...-inch (25.4-cm) square or 12-inch (30.5-cm) diamond mesh throughout the codend for at least 45... gillnets used by a vessel fishing under a monkfish DAS is 10-inch (25.4-cm) diamond mesh, unless otherwise...
Evans, Robert M.
1976-10-05
1. A neutronic reactor having a moderator, coolant tubes traversing the moderator from an inlet end to an outlet end, bodies of material fissionable by neutrons of thermal energy disposed within the coolant tubes, and means for circulating water through said coolant tubes characterized by the improved construction wherein the coolant tubes are constructed of aluminum having an outer diameter of 1.729 inches and a wall thickness of 0.059 inch, and the means for circulating a liquid coolant through the tubes includes a source of water at a pressure of approximately 350 pounds per square inch connected to the inlet end of the tubes, and said construction including a pressure reducing orifice disposed at the inlet ends of the tubes reducing the pressure of the water by approximately 150 pounds per square inch.
NASA Technical Reports Server (NTRS)
Sivo, Joseph N.; Peters, Daniel J.
1959-01-01
A rocket engine with an exhaust-nozzle area ratio of 25 was operated at a constant chamber pressure of 600 pounds per square inch absolute over a range of oxidant-fuel ratios at an altitude pressure corresponding to approximately 47,000 feet. At this condition, the nozzle flow is slightly underexpanded as it leaves the nozzle. The altitude simulation was obtained first through the use of an exhaust diffuser coupled with the rocket engine and secondly, in an altitude test chamber where separate exhauster equipment provided the altitude pressure. A comparison of performance data from these two tests has established that a diffuser used with a rocket engine operating at near-design nozzle pressure ratio can be a valid means of obtaining altitude performance data for rocket engines.
NASA Technical Reports Server (NTRS)
Liebert, Curt H.; Ehlers, Robert C.
1961-01-01
Local experimental heat-transfer coefficients were measured in the chamber and throat of a 2400-pound-thrust ammonia-oxygen rocket engine with a nominal chamber pressure of 600 pounds per square inch absolute. Three injector configurations were used. The rocket engine was run over a range of oxidant-fuel ratio and chamber pressure. The injector that achieved the best performance also produced the highest rates of heat flux at design conditions. The heat-transfer data from the best-performing injector agreed well with the simplified equation developed by Bartz at the throat region. A large spread of data was observed for the chamber. This spread was attributed generally to the variations of combustion processes. The spread was least evident, however, with the best-performing injector.
NASA Technical Reports Server (NTRS)
Swett, Clyde C , Jr
1949-01-01
Ignition studies of flowing gases were made to obtain information applicable to ignition problems in gas-turbine and ram-jet aircraft propulsion systems operating at altitude conditions.Spark energies required for ignition of a flowing propane-air mixture were determined for pressure of 2 to 4 inches mercury absolute, gas velocities of 5.0 to 54.2 feet per second, fuel-air ratios of 0.0607 to 0.1245, and spark durations of 1.5 to 24,400 microseconds. The results showed that at a pressure of 3 inches mercury absolute the minimum energy required for ignition occurred at fuel-air ratios of 0.08 to 0.095. The energy required for ignition increased almost linearly with increasing gas velocity. Shortening the spark duration from approximately 25,000 to 125 microseconds decreased the amount of energy required for ignition. A spark produced by the discharge of a condenser directly into the spark gap and having a duration of 1.5 microseconds required ignition energies larger than most of the long-duration sparks.
An Investigation of the Coefficient of Discharge of Liquids Through Small Round Orifices
NASA Technical Reports Server (NTRS)
Joachim, W F
1926-01-01
The work covered by this report was undertaken in connection with a general investigation of fuel injection engine principles as applied to engines for aircraft propulsion, the specific purpose being to obtain information on the coefficient of discharge of small round orifices suitable for use as fuel injection nozzles. Values for the coefficient were determined for the more important conditions of engine service such as discharge under pressures up to 8,000 pounds per square inch, at temperatures between 80 degrees and 180 degrees F. And into air compressed to pressures up to 1,000 pounds per square inch. The results show that the coefficient ranges between 0.62 and 0.88 for the different test conditions between 1,000 and 8,000 pounds per square inch hydraulic pressure. At lower pressures the coefficient increases materially. It is concluded that within the range of these tests and for hydraulic pressures above 1,000 pound per square inch the coefficient does not change materially with pressure or temperature; that it depends considerably upon the liquid, decreases with increase in orifice size, and increases in the case of discharge into compressed air until the compressed-air pressure equals approximately three-tenths of the hydraulic pressure, beyond which pressure ratio it remains practically constant.
46 CFR 160.048-4 - Construction and workmanship.
Code of Federal Regulations, 2011 CFR
2011-10-01
...(e), but no cushion providing less than 225 square inches of top surface area or measuring less than..., and all buoyant cushions 2 inches thick which are of shapes different from those covered by paragraph... not less than 8 pounds when one inch strips cut across and perpendicular to the seams are pulled apart...
Method and mold for casting thin metal objects
Pehrson, Brandon P; Moore, Alan F
2014-04-29
Provided herein are various embodiments of systems for casting thin metal plates and sheets. Typical embodiments include layers of mold cavities that are oriented vertically for casting the metal plates. In some embodiments, the mold cavities include a beveled edge such that the plates that are cast have a beveled edge. In some embodiments, the mold cavities are filled with a molten metal through an open horizontal edge of the cavity. In some embodiments, the mold cavities are filled through one or more vertical feed orifices. Further disclosed are methods for forming a thin cast metal plate or sheet where the thickness of the cast part is in a range from 0.005 inches to 0.2 inches, and the surface area of the cast part is in a range from 16 square inches to 144 square inches.
Method for casting thin metal objects
Pehrson, Brandon P; Moore, Alan F
2015-04-14
Provided herein are various embodiments of systems for casting thin metal plates and sheets. Typical embodiments include layers of mold cavities that are oriented vertically for casting the metal plates. In some embodiments, the mold cavities include a beveled edge such that the plates that are cast have a beveled edge. In some embodiments, the mold cavities are filled with a molten metal through an open horizontal edge of the cavity. In some embodiments, the mold cavities are filled through one or more vertical feed orifices. Further disclosed are methods for forming a thin cast metal plate or sheet where the thickness of the cast part is in a range from 0.005 inches to 0.2 inches, and the surface area of the cast part is in a range from 16 square inches to 144 square inches.
Stand Alone Pressure Measurement Device (SAPMD) for the space shuttle Orbiter, part 1
NASA Technical Reports Server (NTRS)
Tomlinson, Bill
1989-01-01
The specifications for the Stand Alone Pressure Measurement Device (SAPMD) are as follows: the SAPMD shall measure ambient pressure at the surface of the Orbiter TPS in the range of 0 to 15 pounds per square inch absolute (PSIA). Measurement will begin at solid rocket booster (SRB) ignition as sensed by appropriate vibration sensing elements in the SAPMD. Pressure and corresponding real-time data are to be recorded every one tenth second for 140 seconds and at the end of the recording period, the operation will be discontinued with the data preserved for interrogation subsequent to Orbiter re-entry and landing. The type and size of the battery shall be such as to allow the vibration sensing elements and a real-time clock to be initialized a minimum of 30 day prior to launch and still provide power as necessary to perform the 140 second data recording period after SRB ignition. Battery installation shall be in such a manner as to allow battery replacement without removing the SAPMD from its position or removing more than one TPS tile. The SAPMD must be mounted in specific locations under tile of the TPS. To accommodate such mounting, the absolute maximum physical dimensions much not exceed 6.0 inches in length, 1.5 inches in width, and 0.4 inches in height, and the device shall be of such configuration that it can be bonded to the Orbiter skin at the joint line of two TPS tiles with the pressure sensing port at the surface of the tile. The SAPMD must remain operational in the temperature range of -40 to +85 C and survive storage temperature of -55 to +125 C. The pressure port must withstand 934 C without causing damage to the TPS during entry and must remain functional at 262 C during ascent. The accuracy of the pressure measurement must be plus or minus one-half PSIA over a temperature range of 0 to +36 C. All the specifications were met and verified by prototype testing and documented in the enclosed test data. Four flight-qualified models were fabricated and of these, two were delivered and successfully flown in the cargo bay of STS-26.
NASA Technical Reports Server (NTRS)
Mclellan, Charles H; Bertram, Mitchel H; Moore, John A
1957-01-01
The results of pressure-distribution and force tests of four wings at a Mach number of about 6.9 and a Reynolds number of 0.98 x 10(6) in the Langley 11-inch hypersonic tunnel are presented. The wings had a square plan form, a 5-percent-chord maximum thickness, and diamond, half-diamond, wedge, and half-circular sections.
NASA Astrophysics Data System (ADS)
Mitra, Ashis; Majumdar, Prabal Kumar; Bannerjee, Debamalya
2013-03-01
This paper presents a comparative analysis of two modeling methodologies for the prediction of air permeability of plain woven handloom cotton fabrics. Four basic fabric constructional parameters namely ends per inch, picks per inch, warp count and weft count have been used as inputs for artificial neural network (ANN) and regression models. Out of the four regression models tried, interaction model showed very good prediction performance with a meager mean absolute error of 2.017 %. However, ANN models demonstrated superiority over the regression models both in terms of correlation coefficient and mean absolute error. The ANN model with 10 nodes in the single hidden layer showed very good correlation coefficient of 0.982 and 0.929 and mean absolute error of only 0.923 and 2.043 % for training and testing data respectively.
NASA Technical Reports Server (NTRS)
Fortini, Anthony; Hendrix, Charles D.; Huff, Vearl N.
1959-01-01
The performance for four altitudes (sea-level, 51,000, 65,000, and 70,000 ft) of a rocket engine having a nozzle area ratio of 48.39 and using JP-4 fuel and liquid oxygen as a propellant was evaluated experimentally by use of a 1000-pound-thrust engine operating at a chamber pressure of 600 pounds per square inch absolute. The altitude environment was obtained by a rocket-ejector system which utilized the rocket exhaust gases as the pumping fluid of the ejector. Also, an engine having a nozzle area ratio of 5.49 designed for sea level was tested at sea-level conditions. The following table lists values from faired experimental curves at an oxidant-fuel ratio of 2.3 for various approximate altitudes.
29 CFR 1910.124 - General requirements for dipping and coating operations.
Code of Federal Regulations, 2013 CFR
2013-07-01
...) Chemical reaction. (c) What requirements must I follow to recirculate exhaust air into the workplace? (1... inch (18 mm) thick with a quick-opening valve and carrying a pressure of 25 pounds per square inch (1...
Dimension Yields from Yellow-Poplar Lumber.
1984-06-01
the poor SP Split (includes end checks longer face and then on the good face. than 4 in.) - - The boards and each of their SW Sapwood + + defects were...Cutting Size Random SA = surface area of cutting width Adjustment Adjusted Y-ekd in square inches Length Width reading reading Using the previous...cutting sizes from 4 4 surface area of a 57- by 4-inch FAS yellow-poplar lumber cutting is 1.583 square feet: 3551.58 = 224 cuttings per 1.000 Cutting
Forced-convection Heat Transfer to Water at High Pressures and Temperatures in the Nonboiling Region
NASA Technical Reports Server (NTRS)
Kaufman, S J; Henderson, R W
1951-01-01
Forced-convection heat-transfer data have been obtained for water flowing in an electrically heated tube of circular cross section at water pressures of 200 and 2000 pounds per square inch, and temperatures in the nonboiling region, for water velocities ranging between 5 and 25 feet per second. The results indicate that conventional correlations can be used to predict heat-transfer coefficients for water at pressures up to 2000 pounds per square inch and temperatures in the nonboiling region.
16 CFR 500.12 - Measurement of commodities by length and width, how expressed.
Code of Federal Regulations, 2010 CFR
2010-01-01
... remainder in inches or common or decimal fractions of the yard or foot except that a dimension of less than... dimension of less than 2 feet (60.96 cm) may be stated in inches. (4) For any commodity for which the... square foot (929 cm2) be expressed in terms of length and width in linear measure. The customary inch...
A Moiré Pattern-Based Thread Counter
ERIC Educational Resources Information Center
Reich, Gary
2017-01-01
Thread count is a term used in the textile industry as a measure of how closely woven a fabric is. It is usually defined as the sum of the number of warp threads per inch (or cm) and the number of weft threads per inch. (It is sometimes confusingly described as the number of threads per square inch.) In recent years it has also become a subject of…
ERIC Educational Resources Information Center
Helmreich, James E.; Krog, K. Peter
2018-01-01
We present a short, inquiry-based learning course on concepts and methods underlying ordinary least squares (OLS), least absolute deviation (LAD), and quantile regression (QR). Students investigate squared, absolute, and weighted absolute distance functions (metrics) as location measures. Using differential calculus and properties of convex…
21 CFR 177.1315 - Ethylene-1, 4-cyclohexylene dimethylene terephthalate copolymers.
Code of Federal Regulations, 2014 CFR
2014-04-01
... specified temperatures and times (expressed in micrograms of the terephthaloyl moletles/square centimeter of... 100 milliliters (1) 0.23 microgram per square centimeter (1.5 micrograms per square inch) of food... °F). No thermal treatment in the container. ......do (2) 0.23 microgram per square centimeter (1.5...
Code of Federal Regulations, 2012 CFR
2012-10-01
... south of 66° South latitude must be assumed to be at least: (1) 6.14 pounds per square foot (30 Kilograms per square meter) of horizontal projected area which corresponds to a thickness of 1.3 inches (33 millimeters); and (2) 3.07 pounds per square foot (15 Kilograms per square meter) of vertical projected area...
10 CFR 32.101 - Schedule B-prototype tests for luminous safety devices for use in aircraft.
Code of Federal Regulations, 2010 CFR
2010-01-01
... within the device, or water entering the device, shall be considered leakage. (f) Observations. After... inches of water for 24 hours and shall show no visible evidence of water entry. Absolute pressure of the air above the water shall then be reduced to 1 inch of mercury. Lowered pressure shall be maintained...
10 CFR 32.101 - Schedule B-prototype tests for luminous safety devices for use in aircraft.
Code of Federal Regulations, 2011 CFR
2011-01-01
..., or turbo-propeller engines or to be mounted directly on gas-turbine engines. The device shall be... inches of water for 24 hours and shall show no visible evidence of water entry. Absolute pressure of the air above the water shall then be reduced to 1 inch of mercury. Lowered pressure shall be maintained...
Cecil, L.D.
1988-01-01
The Furnace Creek basin is an area of 8.95 square miles, about three- fourths of which is underlain by metamorphic rocks of low permeability. Reported yields for 14 wells in these rocks range from 1 to 60 gal/min (gallons per minute), with a median of 7.5 gal/min. The northern part of the study area consists of highly permeable carbonate rocks. Nondomestic wells in these rocks typically yield from 200 to 300 gal/min and one well yields 1,200 gal/min. Ground-water discharge from a 4.18-square-mile drainage area underlain by Precambrian granitic and hornblende gneiss averaged 868,000 gallons per day per square mile from October 1983 through September 1985. Thus, as much as 3,630,000 gallons per day could be pumped from wells in this area on a sustained basis. However, pumping this amount would have major adverse effects on streamflow. A water-budget analysis for March 1984 to February 1985 showed that precipitation was 52.16 inches, streamflow was 26.38 inches, evapotranspiration was 29.29 inches, ground-water storage decreased by 5.94 inches and diversions made by Womelsdorf-Robesonia Joint Authority for water supply totaled 2.43 inches. Precipitation during this period was above normal. Four of 18 wells sampled for water quality had iron, manganese, or nitrate concentrations above the U.S. Environmental Protection Agency's recommended limits. The crystalline rocks in the study area yield soft to moderately hard water that is generally acidic.
Effect of Combustion-chamber Shape on the Performance of a Prechamber Compression-ignition Engine
NASA Technical Reports Server (NTRS)
Moore, C S; Collins, J H , Jr
1934-01-01
The effect on engine performance of variations in the shape of the prechamber, the shape and direction of the connecting passage, the chamber volume using a tangential passage, the injection system, and the direction od the fuel spray in the chamber was investigated using a 5 by 7 inch single-cylinder compression-ignition engine. The results show that the performance of this engine can be considerably improved by selecting the best combination of variables and incorporating them in a single design. The best combination as determined from these tests consisted of a disk-shaped chamber connected to the cylinder by means of a flared tangential passage. The fuel was injected through a single-orifice nozzle directed normal to the air swirl and in the same plane. At an engine speed of 1,500 r.p.m. and with the theoretical fuel quantity for no excess air, the engine developed a brake mean effective pressure of 115 pounds per square inch with a fuel consumption of 0.49 pound per brake horsepower-hour and an explosion pressure of 820 pounds per square inch. A brake mean effective pressure of 100 pounds per square inch with a brake-fuel consumption of 0.44 pound per horsepower-hour at 1,500 r.p.m. was obtained.
21 CFR 177.1670 - Polyvinyl alcohol film.
Code of Federal Regulations, 2014 CFR
2014-04-01
... extractives not to exceed 0.078 milligram per square centimeter (0.5 milligram per square inch) of food... the American Society for Testing Materials, 100 Barr Harbor Dr., West Conshohocken, Philadelphia, PA...
16 CFR 1611.36 - Application of act to particular types of products.
Code of Federal Regulations, 2010 CFR
2010-01-01
...) inches on any side or not exceeding five hundred seventy-six (576) square inches in area are not deemed... other factor, a piece of cloth of a finished type or any other product of a finished type appears to be...
Boosted performance of a compression-ignition engine with a displaced piston
NASA Technical Reports Server (NTRS)
Moore, Charles S; Foster, Hampton H
1936-01-01
Performance tests were made using a rectangular displacer arranged so that the combustion air was forced through equal passages at either end of the displacer into the vertical-disk combustion chamber of a single-cylinder, four-stroke-cycle compression-ignition test engine. After making tests to determine optimum displacer height, shape, and fuel-spray arrangement, engine-performance tests were made at 1,500 and 2,000 r.p.m. for a range of boost pressures from 0 to 20 inches of mercury and for maximum cylinder pressures up to 1,150 pounds per square inch. The engine operation for boosted conditions was very smooth, there being no combustion shock even at the highest maximum cylinder pressures. Indicated mean effective pressures of 240 pounds per square inch for fuel consumptions of 0.39 pound per horsepower-hour have been readily reproduced during routine testing at 2,000 r.p.m. at a boost pressure of 20 inches of mercury.
ERIC Educational Resources Information Center
Shibayama, Guy T.
As part of a 90-hour community college course in sheet metal working, this 50-minute lesson was designed to enable a student to: (1) identify and use right and left hand aviation snips; (2) cut out a 6-inch round opening in a piece of sheet metal using aviation snips; and (3) cut out a 6-by-6 inch square opening in a piece of sheet metal using…
Elastomers for Service as Seals for Engine Lubricants and Hydraulic Fluids
1976-02-01
mm NBR PNF psi - fluorocarbon rubber - hour per degrees Fahrenheit - inch-pound per cubic inch - minute per degrees Fahrenheit - milliliter...millimeter - nitrile-butadiene rubber - polyffluoroalkoxy)phosphazene - pounds per square inch t I (1 MAT-75-78 <V ■ >«..*, njf:~-. I...I I I I I I r i. L I I 1 ! «WJBDXNB PA« BUNUfOT FIIMID BACKGROUND Nitrile-butadiene robber ( NBR ) O-nngs have had an accept
Code of Federal Regulations, 2010 CFR
2010-01-01
... expressed: Provided: (a) The quantity of contents for full skins is expressed in terms of square feet with any remainder in terms of the common or decimal fraction of the square foot. (b) The quantity of contents for cut skins of any configuration is expressed in terms of square inches and fractions thereof...
Code of Federal Regulations, 2011 CFR
2011-01-01
... expressed: Provided: (a) The quantity of contents for full skins is expressed in terms of square feet with any remainder in terms of the common or decimal fraction of the square foot. (b) The quantity of contents for cut skins of any configuration is expressed in terms of square inches and fractions thereof...
Code of Federal Regulations, 2013 CFR
2013-01-01
... expressed: Provided: (a) The quantity of contents for full skins is expressed in terms of square feet with any remainder in terms of the common or decimal fraction of the square foot. (b) The quantity of contents for cut skins of any configuration is expressed in terms of square inches and fractions thereof...
Code of Federal Regulations, 2012 CFR
2012-01-01
... expressed: Provided: (a) The quantity of contents for full skins is expressed in terms of square feet with any remainder in terms of the common or decimal fraction of the square foot. (b) The quantity of contents for cut skins of any configuration is expressed in terms of square inches and fractions thereof...
Code of Federal Regulations, 2014 CFR
2014-01-01
... expressed: Provided: (a) The quantity of contents for full skins is expressed in terms of square feet with any remainder in terms of the common or decimal fraction of the square foot. (b) The quantity of contents for cut skins of any configuration is expressed in terms of square inches and fractions thereof...
Installing Juno Radiation Vault
2010-07-12
Technicians installed a special radiation vault onto the propulsion module of NASA Juno spacecraft. Each titanium wall measures nearly a square meter nearly 10 square feet in area and about 1 centimeter a third of an inch in thickness.
Ship Dynamics in the Surf Zone Model Testing
2008-07-01
was implemented for ease of transportation and ease of assembly. Each module was 10 feet square consisting of oriented strand board ( OSB ) plywood with...frame, constructed of 2 inch by 4 inch by 10 feet pieces of wood, was measured, cut, laid, and screwed together for each module. Pieces of OSB
Study of thermal insulation for airborne liquid hydrogen fuel tanks
NASA Technical Reports Server (NTRS)
Ruccia, F. E.; Lindstrom, R. S.; Lucas, R. M.
1978-01-01
A concept for a fail-safe thermal protection system was developed. From screening tests, approximately 30 foams, adhesives, and reinforcing fibers using 0.3-meter square liquid nitrogen cold plate, CPR 452 and Stafoam AA1602, both reinforced with 10 percent by weight of 1/16 inch milled OCF Style 701 Fiberglas, were selected for further tests. Cyclic tests with these materials in 2-inch thicknesses bonded on a 0.6-meter square cold plate with Crest 7410 adhesive systems, were successful. Zero permeability gas barriers were identified and found to be compatible with the insulating concept.
Military Potential Test of Elapsed-Time Indicator, P/N 85986X
1967-06-13
consisting basically of an electrolytic mercury cell, an accutron-quality mercury battery, and a pressure switch . The unit weighs 1. 687 ounces. Installed, it...orientation from 18 inches’ distance. The test item is actuated by a pressure switch which senses an actuating pressure of 40 t 5 pounds per square inch
Diagnostic and Treatment Innovations for Mass Casualties
2016-08-01
measurement * U.S. Customary Units Multiply by International Units Divide by † Length/ Area /Volume inch (in) 2.54 × 10 –2 meter (m) foot...cal) (thermochemical) 4.184 joule (J) Pressure atmosphere (atm) 1.013 250 × 10 5 pascal (Pa) pound force per square inch (psi) 6.984 757 × 10
1998-08-10
In the Tile Fabrication Shop, Tony Rollins, with United Space Alliance, cuts a High-Temperature Reusable Surface Insulation (HRSI) tile on a gun stock contour milling machine. About 70 percent of a Space Shuttle orbiter’s external surface is shielded from heat by a network of more than 24,000 tiles formed from a silica fiber compound. HRSI tiles cover the lower surface of the orbiter, areas around the forward windows, upper body flap, the base heat shield, the "eyeballs" on the front of the Orbital Maneuvering System (OMS) pods, and the leading and trailing edges of the vertical stabilizer and the rudder speed brake. They are generally 6 inches square, but may also be as large as 12 inches square in some areas, and 1 to 5 inches thick. More advanced materials such as Flexible Insulation Blankets have replaced tiles on some upper surfaces of the orbiter
Harris, David Dell; Williams, Robert Charles
1971-01-01
Data collected during the prelogging period 1959-65 indicate an average annual runoff for Needle Branch and Deer and Flynn Creeks of 74.2, 75.1, and 77.7 inches, respectively. The measured precipitation at Flynn Creek of 92.9 inches was 5 inches less than at either Needle Branch or Deer Creek. Unit flood runoff during the prelogging period was found to be lowest on Flynn Creek and highest on Needle Branch. On Needle Branch, there appear to be two distinct low-flow patterns, one for a saturated and one for an unsaturated soil condition. The average annual sediment yield was highest on Flynn Creek, 321 tons per square mile, and lowest on Needle Branch, 166 tons per square mile. Maximum water temperatures were 62?F on Flynn Creek and 61?F on Needle Branch and Deer Creek.
Tony Rollins prepares a new tile for the Space Shuttle orbiter
NASA Technical Reports Server (NTRS)
1998-01-01
In the Tile Fabrication Shop, Tony Rollins, with United Space Alliance, cuts a High-Temperature Reusable Surface Insulation (HRSI) tile on a gun stock contour milling machine. About 70 percent of a Space Shuttle orbiter's external surface is shielded from heat by a network of more than 24,000 tiles formed from a silica fiber compound. HRSI tiles cover the lower surface of the orbiter, areas around the forward windows, upper body flap, the base heat shield, the 'eyeballs' on the front of the Orbital Maneuvering System (OMS) pods, and the leading and trailing edges of the vertical stabilizer and the rudder speed brake. They are generally 6 inches square, but may also be as large as 12 inches square in some areas, and 1 to 5 inches thick. More advanced materials such as Flexible Insulation Blankets have replaced tiles on some upper surfaces of the orbiter.
21 CFR 177.1315 - Ethylene-1, 4-cyclohexylene dimethylene terephthalate copolymers.
Code of Federal Regulations, 2013 CFR
2013-04-01
... terephthaloyl moletles/square centimeter of food-contact surface) Test for orientability Conditions of use 1... solution expressed in grams per 100 milliliters (1) 0.23 microgram per square centimeter (1.5 micrograms per square inch) of food-contact surface when extracted with water added at 82.2 °C (180 °F) and...
49 CFR 172.527 - Background requirements for certain placards.
Code of Federal Regulations, 2011 CFR
2011-10-01
.... (a) Except for size and color, the square background required by § 172.510(a) for certain placards on... requirements of § 172.519 for minimum durability and strength, the square background must consist of a white square measuring 141/4 inches (362.0 mm.) on each side surrounded by a black border extending to 151/4...
49 CFR 172.527 - Background requirements for certain placards.
Code of Federal Regulations, 2014 CFR
2014-10-01
.... (a) Except for size and color, the square background required by § 172.510(a) for certain placards on... requirements of § 172.519 for minimum durability and strength, the square background must consist of a white square measuring 141/4 inches (362.0 mm.) on each side surrounded by a black border extending to 151/4...
21 CFR 177.1315 - Ethylene-1, 4-cyclohexylene dimethylene terephthalate copolymers.
Code of Federal Regulations, 2011 CFR
2011-04-01
... terephthaloyl moletles/square centimeter of food-contact surface) Test for orientability Conditions of use 1... solution expressed in grams per 100 milliliters (1) 0.23 microgram per square centimeter (1.5 micrograms per square inch) of food-contact surface when extracted with water added at 82.2 °C (180 °F) and...
21 CFR 177.1315 - Ethylene-1, 4-cyclohexylene dimethylene terephthalate copolymers.
Code of Federal Regulations, 2012 CFR
2012-04-01
... terephthaloyl moletles/square centimeter of food-contact surface) Test for orientability Conditions of use 1... solution expressed in grams per 100 milliliters (1) 0.23 microgram per square centimeter (1.5 micrograms per square inch) of food-contact surface when extracted with water added at 82.2 °C (180 °F) and...
49 CFR 172.527 - Background requirements for certain placards.
Code of Federal Regulations, 2013 CFR
2013-10-01
.... (a) Except for size and color, the square background required by § 172.510(a) for certain placards on... requirements of § 172.519 for minimum durability and strength, the square background must consist of a white square measuring 141/4 inches (362.0 mm.) on each side surrounded by a black border extending to 151/4...
49 CFR 172.527 - Background requirements for certain placards.
Code of Federal Regulations, 2010 CFR
2010-10-01
.... (a) Except for size and color, the square background required by § 172.510(a) for certain placards on... requirements of § 172.519 for minimum durability and strength, the square background must consist of a white square measuring 141/4 inches (362.0 mm.) on each side surrounded by a black border extending to 151/4...
49 CFR 172.527 - Background requirements for certain placards.
Code of Federal Regulations, 2012 CFR
2012-10-01
.... (a) Except for size and color, the square background required by § 172.510(a) for certain placards on... requirements of § 172.519 for minimum durability and strength, the square background must consist of a white square measuring 141/4 inches (362.0 mm.) on each side surrounded by a black border extending to 151/4...
40 CFR 61.03 - Units and abbreviations.
Code of Federal Regulations, 2012 CFR
2012-07-01
... m=meter m2=square meter m3=cubic meter mg=milligram=10−3gram mm=millimeter=10−3meter Mg=megagram... per minute cc=cubic centimeter Ci=curie d=day °F=degree Fahrenheit ft2=square feet ft3=cubic feet gal... square inch gage °R=degree Rankine µl=microliter=10−6liter v/v=volume per volume yd2=square yards yr=year...
40 CFR 61.03 - Units and abbreviations.
Code of Federal Regulations, 2010 CFR
2010-07-01
... m=meter m2=square meter m3=cubic meter mg=milligram=10−3gram mm=millimeter=10−3meter Mg=megagram... per minute cc=cubic centimeter Ci=curie d=day °F=degree Fahrenheit ft2=square feet ft3=cubic feet gal... square inch gage °R=degree Rankine µl=microliter=10−6liter v/v=volume per volume yd2=square yards yr=year...
40 CFR 61.03 - Units and abbreviations.
Code of Federal Regulations, 2013 CFR
2013-07-01
... m=meter m2=square meter m3=cubic meter mg=milligram=10−3gram mm=millimeter=10−3meter Mg=megagram... per minute cc=cubic centimeter Ci=curie d=day °F=degree Fahrenheit ft2=square feet ft3=cubic feet gal... square inch gage °R=degree Rankine µl=microliter=10−6liter v/v=volume per volume yd2=square yards yr=year...
40 CFR 61.03 - Units and abbreviations.
Code of Federal Regulations, 2011 CFR
2011-07-01
... m=meter m2=square meter m3=cubic meter mg=milligram=10−3gram mm=millimeter=10−3meter Mg=megagram... per minute cc=cubic centimeter Ci=curie d=day °F=degree Fahrenheit ft2=square feet ft3=cubic feet gal... square inch gage °R=degree Rankine µl=microliter=10−6liter v/v=volume per volume yd2=square yards yr=year...
40 CFR 61.03 - Units and abbreviations.
Code of Federal Regulations, 2014 CFR
2014-07-01
... m=meter m2=square meter m3=cubic meter mg=milligram=10−3gram mm=millimeter=10−3meter Mg=megagram... per minute cc=cubic centimeter Ci=curie d=day °F=degree Fahrenheit ft2=square feet ft3=cubic feet gal... square inch gage °R=degree Rankine µl=microliter=10−6liter v/v=volume per volume yd2=square yards yr=year...
7 CFR 52.774 - Fill of container.
Code of Federal Regulations, 2012 CFR
2012-01-01
... No. 8 circular sieve of proper diameter containing eight meshes to the inch (0.0937 inch (2.3 mm), ±3 percent, square openings) so as to distribute the product evenly over the sieve. Without shifting the product, incline the sieve at an angle of 17° to 20° to facilitate drainage and allow to drain for two...
7 CFR 52.774 - Fill of container.
Code of Federal Regulations, 2010 CFR
2010-01-01
... No. 8 circular sieve of proper diameter containing eight meshes to the inch (0.0937 inch (2.3 mm), ±3 percent, square openings) so as to distribute the product evenly over the sieve. Without shifting the product, incline the sieve at an angle of 17° to 20° to facilitate drainage and allow to drain for two...
7 CFR 52.774 - Fill of container.
Code of Federal Regulations, 2011 CFR
2011-01-01
... No. 8 circular sieve of proper diameter containing eight meshes to the inch (0.0937 inch (2.3 mm), ±3 percent, square openings) so as to distribute the product evenly over the sieve. Without shifting the product, incline the sieve at an angle of 17° to 20° to facilitate drainage and allow to drain for two...
Code of Federal Regulations, 2014 CFR
2014-01-01
... one-half of a square inch on the midrib portion of the branch or branches. (c) Growth cracks, when the stalk has more than one branch affected by growth cracks any of which are more than one-half inch long... are more than five hair-like lines of any length on one or more heart branches, or when there is more...
Code of Federal Regulations, 2013 CFR
2013-01-01
... one-half of a square inch on the midrib portion of the branch or branches. (c) Growth cracks, when the stalk has more than one branch affected by growth cracks any of which are more than one-half inch long... are more than five hair-like lines of any length on one or more heart branches, or when there is more...
46 CFR 54.30-5 - Limitations and requirements.
Code of Federal Regulations, 2011 CFR
2011-10-01
... pounds per square inch, thickness of shell is not greater than 1 inch, and the design temperature is not greater than 115 °F. (3) It will carry liquids of specific gravity no greater than 1.05. (4) Design... designs involving the following types of welded connections shown in UW-16.1 of section VIII of the ASME...
46 CFR 54.30-5 - Limitations and requirements.
Code of Federal Regulations, 2010 CFR
2010-10-01
... pounds per square inch, thickness of shell is not greater than 1 inch, and the design temperature is not greater than 115 °F. (3) It will carry liquids of specific gravity no greater than 1.05. (4) Design... designs involving the following types of welded connections shown in UW-16.1 of section VIII of the ASME...
46 CFR 54.30-5 - Limitations and requirements.
Code of Federal Regulations, 2013 CFR
2013-10-01
... pounds per square inch, thickness of shell is not greater than 1 inch, and the design temperature is not greater than 115 °F. (3) It will carry liquids of specific gravity no greater than 1.05. (4) Design... designs involving the following types of welded connections shown in UW-16.1 of section VIII of the ASME...
46 CFR 54.30-5 - Limitations and requirements.
Code of Federal Regulations, 2014 CFR
2014-10-01
... pounds per square inch, thickness of shell is not greater than 1 inch, and the design temperature is not greater than 115 °F. (3) It will carry liquids of specific gravity no greater than 1.05. (4) Design... designs involving the following types of welded connections shown in UW-16.1 of section VIII of the ASME...
46 CFR 54.30-5 - Limitations and requirements.
Code of Federal Regulations, 2012 CFR
2012-10-01
... pounds per square inch, thickness of shell is not greater than 1 inch, and the design temperature is not greater than 115 °F. (3) It will carry liquids of specific gravity no greater than 1.05. (4) Design... designs involving the following types of welded connections shown in UW-16.1 of section VIII of the ASME...
VizieR Online Data Catalog: Ultraviolet Excess Galaxies (Mitchell+ 1982)
NASA Astrophysics Data System (ADS)
Mitchell, K. J.; Brotzman, L. E.; Warnock, A.; Usher, P. D.
2015-05-01
The catalog contains a list of 412 faint galaxies selected for their apparent ultraviolet excess. The galaxies were selected from a 3-color (UBV) plate taken with the Palomar 48-inch Schmidt telescope. The 14-inch-square plates cover an area of 30 square degrees centered on Kapteyn Selected Area 28. The catalog includes running numbers, coordinates, color codes, magnitude codes, morphologies, diameters, and notes. The catalogued galaxies were selected by eye from the Palomar Schmidt 3-color (UBV) plate PS24771, centered on Kapteyn Selexted Area 28 and taken by Usher under conditions of good seeing and transparency. (1 data file).
Static, Drop, and Flight Tests on Musselman Type Airwheels
NASA Technical Reports Server (NTRS)
Peck, William C; Beard, Albert P
1932-01-01
The purpose of this investigation was to obtain quantitative information on the shock-reducing and energy-dissipating qualities of a set of 30 by 13-6 Musselman type airwheels. The investigation consisted of static, drop, and flight tests. The static tests were made with inflation pressures of approximately 0, 5, 10, 15, 20, and 25 pounds per square inch and loadings up to 9,600 pounds. The drop tests were with the inflation pressures approximately 5, 10, 15, 20, and 25 pounds per square inch and loadings of 1,840, 2,440, 3,050, and 3,585 pounds. The flight tests were made with VE-7 airplane weighing 2,153 pounds, with the tires inflated to 5, 10, and 15 pounds per square inch. The landing gears used in conjunction with airwheels were practically rigid structures. The results of the tests showed that the walls of the tires carried a considerable portion of the load, each tire supporting a load of 600 pounds with a depression of approximately 6 inches. The shock-reducing qualities, under severe tests, and the energy dissipating characteristics of the tires, under all tests, were poor. The latter was evidenced by the rebound present in all landings made. In the severe drop tests, the free rebound reached as much as 60 per cent of the free drop. The results indicate that a shock-reducing and energy-dissipating mechanism should be used in conjunction with airwheels.
49 CFR 172.327 - Petroleum sour crude oil in bulk packaging.
Code of Federal Regulations, 2014 CFR
2014-10-01
... least 100 mm (3.9 inches). The width of the border forming the square-on-point marking must be at least... hydrogen sulfide vapors may occur. (b) The border of the square-on-point must be black or red on a white or other suitable contrasting background. The symbol must be black and located in the center of the square...
CFD Simulations for Arc-Jet Panel Testing Capability Development Using Semi-Elliptical Nozzles
NASA Technical Reports Server (NTRS)
Gokcen, Tahir; Balboni, John A.; Hartman, G. Joseph
2016-01-01
This paper reports computational simulations in support of arc-jet panel testing capability development using semi-elliptical nozzles in a high enthalpy arc-jet facility at NASA Ames Research Center. Two different semi-elliptical nozzle configurations are proposed for testing panel test articles. Computational fluid dynamics simulations are performed to provide estimates of achievable panel surface conditions and useful test area for each configuration. The present analysis comprises three-dimensional simulations of the nonequilibrium flowfields in the semi-elliptical nozzles, test box and flowfield over the panel test articles. Computations show that useful test areas for the proposed two nozzle options are 20.32 centimeters by 20.32 centimeters (8 inches by 8 inches) and 43.18 centimeters by 43.18 centimeters (17 inches by 17 inches). Estimated values of the maximum cold-wall heat flux and surface pressure are 155 watts per centimeters squared and 39 kilopascals for the smaller panel test option, and 44 watts per centimeters squared and 7 kilopascals for the larger panel test option. Other important properties of the predicted flowfields are presented, and factors that limit the useful test area in the semi-free jet test configuration are discussed.
1. RESTORED GLOVER LOCOMOTIVE #81421 JUST WEST OF MARIETTA SQUARE; ...
1. RESTORED GLOVER LOCOMOTIVE #81421 JUST WEST OF MARIETTA SQUARE; 36 INCH GAUGE 2-6-0, BUILT 1-3-17. RETURNED FOR REPAIR AND RESALE IN 1923, LAST OFFERED FOR SALE IN 1931 FOR $750. - Glover Machine Works, 651 Butler Street, Marietta, Cobb County, GA
NASA Technical Reports Server (NTRS)
Ball, J. W.; Klug, G. W.
1976-01-01
Results from tests in the NASA/CF4, 20 inch Mach 6 and the 22 inch Helium Tunnel consist of pressure measurements on the lower surfaces of the Rockwell Space Shuttle Orbiter. All data are in absolute pressures. Data were recorded with the model at a Mach number of 6 and 20 at angles of 10 deg to 30 deg.
Crack Growth of D6 Steel in Air and High Pressure Oxygen
NASA Technical Reports Server (NTRS)
Bixler, W. D.; Engstrom, W. L.
1971-01-01
Fracture and subcritical flaw growth characteristics were experimentally determined for electroless nickel plated D6 steel in dry air and high pressure oxygen environments as applicable to the Lunar Module/Environmental Control System (LM/ECS) descent gaseous oxygen (GOX) tank. The material tested included forgings, plate, and actual LM/ECS descent GOX tank material. Parent metal and TIG (tungsten inert gas) welds were tested. Tests indicate that proof testing the tanks at 4000 pounds per square inch or higher will insure safe operation at 3060 pounds per square inch. Although significant flaw growth can occur during proofing, subsequent growth of flaws during normal tank operation is negligible.
46 CFR 108.415 - Fire pump: General.
Code of Federal Regulations, 2013 CFR
2013-10-01
... have at least two independently driven fire pumps that can each deliver water at a continuous pitot tube pressure of at least 3.5 kilograms per square centimeter (approximately 50 pounds per square inch) at least two fire hose nozzles that are connected to the highest two fire hydrants on the unit...
46 CFR 108.415 - Fire pump: General.
Code of Federal Regulations, 2010 CFR
2010-10-01
... have at least two independently driven fire pumps that can each deliver water at a continuous pitot tube pressure of at least 3.5 kilograms per square centimeter (approximately 50 pounds per square inch) at least two fire hose nozzles that are connected to the highest two fire hydrants on the unit...
46 CFR 108.415 - Fire pump: General.
Code of Federal Regulations, 2012 CFR
2012-10-01
... have at least two independently driven fire pumps that can each deliver water at a continuous pitot tube pressure of at least 3.5 kilograms per square centimeter (approximately 50 pounds per square inch) at least two fire hose nozzles that are connected to the highest two fire hydrants on the unit...
46 CFR 108.415 - Fire pump: General.
Code of Federal Regulations, 2011 CFR
2011-10-01
... have at least two independently driven fire pumps that can each deliver water at a continuous pitot tube pressure of at least 3.5 kilograms per square centimeter (approximately 50 pounds per square inch) at least two fire hose nozzles that are connected to the highest two fire hydrants on the unit...
46 CFR 108.415 - Fire pump: General.
Code of Federal Regulations, 2014 CFR
2014-10-01
... have at least two independently driven fire pumps that can each deliver water at a continuous pitot tube pressure of at least 3.5 kilograms per square centimeter (approximately 50 pounds per square inch) at least two fire hose nozzles that are connected to the highest two fire hydrants on the unit...
Combustion Instability in an Acid-Heptane Rocket with a Pressurized-Gas Propellant Pumping System
NASA Technical Reports Server (NTRS)
Tischler, Adelbert O.; Bellman, Donald R.
1951-01-01
Results of experimental measurements of low-frequency combustion instability of a 300-pound thrust acid-heptane rocket engine were compared to the trends predicted by an analysis of combustion instability in a rocket engine with a pressurized-gas propellant pumping system. The simplified analysis, which assumes a monopropellant model, was based on the concept of a combustion the delay occurring from the moment of propellant injection to the moment of propellant combustion. This combustion time delay was experimentally measured; the experimental values were of approximately half the magnitude predicted by the analysis. The pressure-fluctuation frequency for a rocket engine with a characteristic length of 100 inches and operated at a combustion-chamber pressure of 280 pounds per square inch absolute was 38 cycles per second; the analysis indicated. a frequency of 37 cycles per second. Increasing combustion-chamber characteristic length decreased the pressure-fluctuation frequency, in conformity to the analysis. Increasing the chamber operating pressure or increasing the injector pressure drop increased the frequency. These latter two effects are contrary to the analysis; the discrepancies are attributed to the conflict between the assumptions made to simplify the analysis and the experimental conditions. Oxidant-fuel ratio had no apparent effect on the experimentally measured pressure-fluctuation frequency for acid-heptane ratios from 3.0 to 7.0. The frequencies decreased with increased amplitude of the combustion-chamber pressure variations. The analysis indicated that if the combustion time delay were sufficiently short, low-frequency combustion instability would be eliminated.
Hydrologic data for North Creek, Trinity River basin, Texas, 1975
Kidwell, C.C.
1977-01-01
This report contains the rainfall, runoff, and storage data collected during the 1975 water year for the 21.6-square-mile area above the stream-gaging station North Creek near Jacksboro, Texas. The weighted-mean rainfall in the study area during the water year was 39.01 inches, which is greater than the 18-year average of 30.21 inches for the period 1958-75. Monthly rainfall totals ranged from 1.04 inches in November to 7.94 inches in May. The mean discharge for 1975 at the stream-gaging station was 5.98 cfs, compared with the 14-year (1957-70) average of 5.75 cfs. The annual runoff from the basin above the stream-gaging station was 4,330 acre-feet or 3.76 inches. Three storms were selected for detailed computations for the 1975 water year. The storms occurred on Oct. 30-31, 1974, May 2, 1975 , and Aug. 26, 1975. Rainfall and discharge were computed on the basis of a refined time breakdown. Patterns of the storms are illustrated by hydrographs and mass curves. A summary of rainfall-runoff data is tabulated. There are five floodwater-retarding structures in the study area. These structures have a total capacity of 4,425 acre-feet below flood-spillway crests and regulate streamflow from 16.3 square miles, or 75 percent of the study area. A summary of the physical data at each of the floodwater-retarding structures is included. (Woodard-USGS)
21 CFR 177.1670 - Polyvinyl alcohol film.
Code of Federal Regulations, 2013 CFR
2013-04-01
... tables 1 and 2 of § 176.170(c) of this chapter, yields total extractives not to exceed 0.078 milligram per square centimeter (0.5 milligram per square inch) of food-contact surface when tested by ASTM... Materials,” which is incorporated by reference. Copies may be obtained from the American Society for Testing...
21 CFR 177.1670 - Polyvinyl alcohol film.
Code of Federal Regulations, 2012 CFR
2012-04-01
... tables 1 and 2 of § 176.170(c) of this chapter, yields total extractives not to exceed 0.078 milligram per square centimeter (0.5 milligram per square inch) of food-contact surface when tested by ASTM... Materials,” which is incorporated by reference. Copies may be obtained from the American Society for Testing...
Forecasting Error Calculation with Mean Absolute Deviation and Mean Absolute Percentage Error
NASA Astrophysics Data System (ADS)
Khair, Ummul; Fahmi, Hasanul; Hakim, Sarudin Al; Rahim, Robbi
2017-12-01
Prediction using a forecasting method is one of the most important things for an organization, the selection of appropriate forecasting methods is also important but the percentage error of a method is more important in order for decision makers to adopt the right culture, the use of the Mean Absolute Deviation and Mean Absolute Percentage Error to calculate the percentage of mistakes in the least square method resulted in a percentage of 9.77% and it was decided that the least square method be worked for time series and trend data.
Floods of May-July 1950 in southeastern Nebraska
,
1953-01-01
Four floods occurred in southeast Nebraska during the period of May to July 1950. Two of these were the greatest known in the State if the size of the drainage areas is considered, and the other two were not so spectacular but were of notable size and of possible hydrologic significance in their relation to the two major floods. Although property loss and damage have been exceeded in previous floods in Nebraska, notably in the flood of May-June 1935 on the Republican River, they were extremely high in the period covered by this report. Loss of life, which resulted largely from the rapid cresting of the streams, was likewise high. Each of the floods was caused by heavy precipitation, which at times reached intensities seldom recorded in the Missouri River basin. On May 8, 1950, more than 14 inches of rain fell over certain areas of the Little Nemaha River basin within a period of a few hours. One center of the storm of July 8, 1950,occurred at York, Nebr., where 11 inches of rain was recorded within a 4-hour period, and the storm total exceeded 13 inches. Notable high rates of discharge produced by the intense rainfall were 1,030 cfs per square mile from 218 square miles of drainage area in the Little Nemaha River basin on May 9, 1950; 1,020 cfs per square mile from 2.5 square miles drainage area in the Elkhorn River basin on June 2, 1950; and 3,320 cfs per square mile from 6.93 square miles of drainage area in the Big Blue River basin on July 9, 1950. This report presents records of stage and discharge for the flood. periods at 36 stream-gaging stations in southeast Nebraska, and a summary of peak discharges, with comparative data for previously known floods at 45 measurement points. The report also includes a discussion of the weather associated with the floods and other data pertinent to the floods.
Effects of size on three-cone bit performance in laboratory drilled shale
DOE Office of Scientific and Technical Information (OSTI.GOV)
Black, A.D.; DiBona, B.G.; Sandstrom, J.L.
1982-09-01
The effects of size on the performance of 3-cone bits were measured during laboratory drilling tests in shale at simulated downhole conditions. Four Reed HP-SM 3-cone bits with diameters of 6 1/2, 7 7/8, 9 1/2 and 11 inches were used to drill Mancos shale with water-based mud. The tests were conducted at constant borehole pressure, two conditions of hydraulic horsepower per square inch of bit area, three conditions of rotary speed and four conditions of weight-on-bit per inch of bit diameter. The resulting penetration rates and torques were measured. Statistical techniques were used to analyze the data.
Design and development of a hard tube flexible radiator system
NASA Technical Reports Server (NTRS)
Hixon, C. W.
1980-01-01
The construction and operational characteristics of an extended life flexible radiator panel is described. The radiator panel consists of a flexible fin laminate and stainless steel flow tubes designed for a 90 percent probability of surviving 5 years in an Earth orbit micrometeoroid environment. The radiator panel rejects 1.1 kW sub t of heat into an environmental sink temperature of 0 F. Total area is 170 square feet and the panel extends 25 feet in the fully deployed position. When retracted the panel rolls onto a 11.5 inch diameter by 52 inch long storage drum, for a final stored diameter of 22 inches.
The effect of advance growth on ponderosa pine seedling mortality at Challenge Experimental Forest
Dale O. Hall
1963-01-01
In seed-tree cuttings at Challenge Experimental Forest, preliminary data show that as advance-growth stocking (20 inches in d.b.h. or less ) increased from 11 t o 49 square feet, seedling mortality increased from 4 to 32 percent (based on stocked mil-acre plots). A comparable increase in the stocking of seed trees over 20 inches in d .b.h. did not increase mortality....
Transverse Diode Pumping of Solid-State Lasers
1992-05-29
more common apertures (laser rod end and cavity end mirror ) leads to a thin-film coating damage issue. The transverse pumped geometry avoids the...proprietary one-half inch square cooler developed for high-power adaptive optics mirror applications. The laser performance observed, with up to 35 watts of...including the development of active mirrors capable of sustaining high power loadings. As part of those efforts, TTC has developed a small (one-half inch
Heat Treatment Investigation of 4330 Vanadium-Modified Steel
1989-08-01
the desired properties, using the results from the tensile and subsized Charpy impact tests on the 1 2-inch-diameter stock our further investigations...for the subsized Charpy specimens is shown graphically in Appendix C as a function of tempering temperature. This data gave a good indication that the... Charpy energy for full-sized specimens (0.394-inch-square cross section) would be near our expected values. Due to the dimensions of the subsized
NASA Technical Reports Server (NTRS)
Carter, David J., Jr.
1960-01-01
An investigation was conducted to determine whether solid-propellant rocket motors could be ignited and destroyed by small-particle impacts at particle velocities up to a approximately 10,940 feet per second. Spheres ranging from 1/16 to 7/32 inch in diameter were fired into simulated rocket motors containing T-22 propellant over a range of ambient pressures from sea level to 0.12 inch of mercury absolute. Simulated cases of stainless steel, aluminum alloy, and laminated Fiberglas varied in thickness from 1/50 to 1/8 inch. Within the scope of this investigation, it was found that ignition and explosive destruction of simulated steel-case rocket motors could result from impacts by steel spheres at the lowest attainable pressure.
Design and Checkout of a High Speed Research Nozzle Evaluation Rig
NASA Technical Reports Server (NTRS)
Castner, Raymond S.; Wolter, John D.
1997-01-01
The High Flow Jet Exit Rig (HFJER) was designed to provide simulated mixed flow turbojet engine exhaust for one- seventh scale models of advanced High Speed Research test nozzles. The new rig was designed to be used at NASA Lewis Research Center in the Nozzle Acoustic Test Rig and the 8x6 Supersonic Wind Tunnel. Capabilities were also designed to collect nozzle thrust measurement, aerodynamic measurements, and acoustic measurements when installed at the Nozzle Acoustic Test Rig. Simulated engine exhaust can be supplied from a high pressure air source at 33 pounds of air per second at 530 degrees Rankine and nozzle pressure ratios of 4.0. In addition, a combustion unit was designed from a J-58 aircraft engine burner to provide 20 pounds of air per second at 2000 degrees Rankine, also at nozzle pressure ratios of 4.0. These airflow capacities were designed to test High Speed Research nozzles with exhaust areas from eighteen square inches to twenty-two square inches. Nozzle inlet flow measurement is available through pressure and temperature sensors installed in the rig. Research instrumentation on High Speed Research nozzles is available with a maximum of 200 individual pressure and 100 individual temperature measurements. Checkout testing was performed in May 1997 with a 22 square inch ASME long radius flow nozzle. Checkout test results will be summarized and compared to the stated design goals.
Low frequency AC waveform generator
Bilharz, Oscar W.
1986-01-01
Low frequency sine, cosine, triangle and square waves are synthesized in circuitry which allows variation in the waveform amplitude and frequency while exhibiting good stability and without requiring significant stabilization time. A triangle waveform is formed by a ramped integration process controlled by a saturation amplifier circuit which produces the necessary hysteresis for the triangle waveform. The output of the saturation circuit is tapped to produce the square waveform. The sine waveform is synthesized by taking the absolute value of the triangular waveform, raising this absolute value to a predetermined power, multiplying the raised absolute value of the triangle wave with the triangle wave itself and properly scaling the resultant waveform and subtracting it from the triangular waveform itself. The cosine is synthesized by squaring the triangular waveform, raising the triangular waveform to a predetermined power and adding the squared waveform raised to the predetermined power with a DC reference and subtracting the squared waveform therefrom, with all waveforms properly scaled. The resultant waveform is then multiplied with a square wave in order to correct the polarity and produce the resultant cosine waveform.
Low frequency ac waveform generator
Bilharz, O.W.
1983-11-22
Low frequency sine, cosine, triangle and square waves are synthesized in circuitry which allows variation in the waveform amplitude and frequency while exhibiting good stability and without requiring significant stablization time. A triangle waveform is formed by a ramped integration process controlled by a saturation amplifier circuit which produces the necessary hysteresis for the triangle waveform. The output of the saturation circuit is tapped to produce the square waveform. The sine waveform is synthesized by taking the absolute value of the triangular waveform, raising this absolute value to a predetermined power, multiplying the raised absolute value of the triangle wave with the triangle wave itself and properly scaling the resultant waveform and subtracting it from the triangular waveform to a predetermined power and adding the squared waveform raised to the predetermined power with a DC reference and subtracting the squared waveform therefrom, with all waveforms properly scaled. The resultant waveform is then multiplied with a square wave in order to correct the polarity and produce the resultant cosine waveform.
Heat Pipe Thermal Conditioning Panel
NASA Technical Reports Server (NTRS)
Saaski, E. W.
1973-01-01
The technology involved in designing and fabricating a heat pipe thermal conditioning panel to satisfy a broad range of thermal control system requirements on NASA spacecraft is discussed. The design specifications were developed for a 30 by 30 inch heat pipe panel. The fundamental constraint was a maximum of 15 gradient from source to sink at 300 watts input and a flux density of 2 watts per square inch. The results of the performance tests conducted on the panel are analyzed.
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.
21 CFR 177.2415 - Poly(aryletherketone) resins.
Code of Federal Regulations, 2012 CFR
2012-04-01
... 12,000, as determined by gel permeation chromatography in comparison with polystyrene standards, and... milligrams per square inch of food contact surface: Distilled water, 50 percent (by volume) ethanol in...
21 CFR 177.2415 - Poly(aryletherketone) resins.
Code of Federal Regulations, 2013 CFR
2013-04-01
... 12,000, as determined by gel permeation chromatography in comparison with polystyrene standards, and... milligrams per square inch of food contact surface: Distilled water, 50 percent (by volume) ethanol in...
21 CFR 177.2415 - Poly(aryletherketone) resins.
Code of Federal Regulations, 2010 CFR
2010-04-01
... 12,000, as determined by gel permeation chromatography in comparison with polystyrene standards, and... milligrams per square inch of food contact surface: Distilled water, 50 percent (by volume) ethanol in...
21 CFR 177.2415 - Poly(aryletherketone) resins.
Code of Federal Regulations, 2011 CFR
2011-04-01
... 12,000, as determined by gel permeation chromatography in comparison with polystyrene standards, and... milligrams per square inch of food contact surface: Distilled water, 50 percent (by volume) ethanol in...
Some Characteristics of Fuel Sprays at Low-injection Pressures
NASA Technical Reports Server (NTRS)
Rothrock, A M; Waldron, C D
1931-01-01
This report presents the results of tests conducted at the Langley Memorial Aeronautical Laboratory, Langley Field, Va., to determine some of the characteristics of the fuel sprays obtained from an 0.008-inch and a 0.020-inch open nozzle when injection pressures from 100 to 500 pounds per square inch were used. Fuel oil and gasoline were injected into air at densities of atmospheric land 0.325 pound per cubic foot. It was found that the penetration rate at these low pressures was about the same as the rate obtained with higher pressures. Spray cone-angles were small and individual oil drops were visible in all the sprays. Gasoline and fuel oil sprays had similar characteristics.
International Space Station (ISS) S-Band Corona Discharge Anomaly Consultation
NASA Technical Reports Server (NTRS)
Kichak, Robert A.; Leidecker, Henning; Battel, Steven; Ruitberg, Arthur; Sank, Victor
2008-01-01
The Assembly and Contingency Radio Frequency Group (ACRFG) onboard the International Space Station (ISS) is used for command and control communications and transmits (45 dBm or 32 watts) and receives at S-band. The system is nominally pressurized with gaseous helium (He) and nitrogen (N2) at 8 pounds per square inch absolute (psia). MacDonald, Dettwiler and Associates Ltd. (MDA) was engaged to analyze the operational characteristics of this unit in an effort to determine if the anomalous behavior was a result of a corona event. Based on this analysis, MDA did not recommend continued use of this ACRFG. The NESC was requested to provide expert support in the area of high-voltage corona and multipactoring in an S-Band RF system and to assess the probability of corona occurring in the ACRFG during the planned EVA. The NESC recommended minimal continued use of S/N 002 ACRFG until a replacement unit can be installed. Following replacement, S/N 002 will be subjected to destructive failure analysis in an effort to determine the proximate and root cause(s) of the anomalous behavior.
Prebreathe Protocol for Extravehicular Activity Technical Consultation Report
NASA Technical Reports Server (NTRS)
Ross, Jerry; Duncan, Michael
2008-01-01
In the performance of EVA by that National Aeronautics and Space Administration (NASA) astronauts, there exists a risk of DCS as the suit pressure is reduced to 4.3 pounds per square inch, absolute (psia) from the International Space Station (ISS) pressure of 14.7 psia. Several DCS-preventive procedures have been developed and implemented. Each of these procedures involve the use of oxygen (O2) prebreathe to effectively washout tissue nitrogen (N2).The management of the ISS Programs convened an expert independent peer review Team to conduct a review of the Decompression Sickness (DCS) risks associated with the Extra Vehicular Activity (EVA) Campout Prebreathe (PB) protocol for its consideration for use on future missions. The major findings and recommendations of the expert panel are: There is no direct experimental data to confirm the potential DCS risks of the Campout PB protocol. However, based on model data, statistical probability, physiology, and information derived from similar PB protocols, there is no compelling evidence to suggest that the Campout PB protocol is less safe than the other NASA approved PB protocols.
Habitat Options to Protect Against Decompression Sickness on Mars
NASA Astrophysics Data System (ADS)
Conkin, J.
2000-07-01
Men and women are alive today, although perhaps still in diapers, who will explore the surface of Mars. Two achievable goals to enable this exploration are to use Martian resources, and to provide a safe means for unrestricted access to the surface. A cost-effective approach for Mars exploration is to use the available resources, such as water and atmospheric gases. Nitrogen (N2) and Argon (Ar) in a concentration ratio of 1.68/1.0 are available, and could form the inert gas component of a habitat atmosphere at 8.0, 9.0, or 10.0 pounds per square inch absolute (psia). The habitat and space suit must be designed as an integrated, complementary, system: a comfortable living environment about 85% of the time and a safe working environment about 15% of the time. A goal is to provide a system that permits unrestricted exploration of Mars. However the risk of decompression sickness (DCS) during the extravehicular activity (EVA) in a 3.75 psia suit after exposure to either of the three habitat conditions may limit unrestricted exploration.
40 CFR 72.3 - Measurements, abbreviations, and acronyms.
Code of Federal Regulations, 2010 CFR
2010-07-01
.... MWe—megawatt electrical. MWge—gross megawatt electrical. NIST—National Institute of Standards and Technology. ppm—parts per million. psi—pounds per square inch. °R—degree Rankine. RATA—relative accuracy test...
10 CFR 590.208 - Small volume exports.
Code of Federal Regulations, 2013 CFR
2013-01-01
... (14.73 pounds per square inch at 60 degrees Fahrenheit) or the liquefied or compressed equivalent thereof, in a single shipment for scientific, experimental, or other non-utility gas use without prior...
10 CFR 590.208 - Small volume exports.
Code of Federal Regulations, 2010 CFR
2010-01-01
... (14.73 pounds per square inch at 60 degrees Fahrenheit) or the liquefied or compressed equivalent thereof, in a single shipment for scientific, experimental, or other non-utility gas use without prior...
10 CFR 590.208 - Small volume exports.
Code of Federal Regulations, 2012 CFR
2012-01-01
... (14.73 pounds per square inch at 60 degrees Fahrenheit) or the liquefied or compressed equivalent thereof, in a single shipment for scientific, experimental, or other non-utility gas use without prior...
10 CFR 590.208 - Small volume exports.
Code of Federal Regulations, 2011 CFR
2011-01-01
... (14.73 pounds per square inch at 60 degrees Fahrenheit) or the liquefied or compressed equivalent thereof, in a single shipment for scientific, experimental, or other non-utility gas use without prior...
10 CFR 590.208 - Small volume exports.
Code of Federal Regulations, 2014 CFR
2014-01-01
... (14.73 pounds per square inch at 60 degrees Fahrenheit) or the liquefied or compressed equivalent thereof, in a single shipment for scientific, experimental, or other non-utility gas use without prior...
40 CFR 72.3 - Measurements, abbreviations, and acronyms.
Code of Federal Regulations, 2012 CFR
2012-07-01
.... MWe—megawatt electrical. MWge—gross megawatt electrical. NIST—National Institute of Standards and Technology. ppm—parts per million. psi—pounds per square inch. °R—degree Rankine. RATA—relative accuracy test...
40 CFR 72.3 - Measurements, abbreviations, and acronyms.
Code of Federal Regulations, 2014 CFR
2014-07-01
.... MWe—megawatt electrical. MWge—gross megawatt electrical. NIST—National Institute of Standards and Technology. ppm—parts per million. psi—pounds per square inch. °R—degree Rankine. RATA—relative accuracy test...
40 CFR 72.3 - Measurements, abbreviations, and acronyms.
Code of Federal Regulations, 2011 CFR
2011-07-01
.... MWe—megawatt electrical. MWge—gross megawatt electrical. NIST—National Institute of Standards and Technology. ppm—parts per million. psi—pounds per square inch. °R—degree Rankine. RATA—relative accuracy test...
40 CFR 72.3 - Measurements, abbreviations, and acronyms.
Code of Federal Regulations, 2013 CFR
2013-07-01
.... MWe—megawatt electrical. MWge—gross megawatt electrical. NIST—National Institute of Standards and Technology. ppm—parts per million. psi—pounds per square inch. °R—degree Rankine. RATA—relative accuracy test...
MM&T for Linear Resonant Cooler. Volume 1
1988-02-16
Tesla *Magnet Material Samarium Cobalt Radially Magnetized Inner Diameter = 1.25" Length = 0.79" Coil Assembly Number of Turns/Section = 90 Outside...Diameter = 1.22" Inside Diameter = 0.86" Inner Iron Material 2 V Permendur Inside Diameter = 0.38" Length 1.84" Design Max. Flux Density = 2.4 Tesla 0 3-12...suspended with rubber bands 60 inches above the floor of the semi -anechoic room. A six foot square piece of 2 inch thick foam was centered on the floor
Short Time Elevated Temperature Tensile Properties and Notch Toughness of Some Chromium-Iron Alloys
1957-06-07
toughness of matcrials A, B, and C was determined by using subsize V-notch Charpy Specimens, 1 inch long by 0.197 inch square prepared with their...elevated temperature tensile tests and V-notch Charpy imapact tests of som recently developed alloys with 4O,’a and 50,,1 ohromiuma are presented in this...lengths parallel to the longitudinal uxis of the alloy bars. In addition, some standard size V-notch Charpy specimens waro mach-ined from material B, for
Code of Federal Regulations, 2010 CFR
2010-01-01
... following regions: Afghanistan, India, Iran, Iraq, Mexico, Nepal, Pakistan, and South Africa. (2) The... solution of hot water and detergent, applied under pressure of at least 30 pounds per square inch, at a...
The Hot-Pressing of Hafnium Carbide (Melting Point, 7030 F)
NASA Technical Reports Server (NTRS)
Sanders, William A.; Grisaffe, Salvatore J.
1960-01-01
An investigation was undertaken to determine the effects of the hot-pressing variables (temperature, pressure, and time) on the density and grain size of hafnium carbide disks. The purpose was to provide information necessary for the production of high-density test shapes for the determination of physical and mechanical properties. Hot-pressing of -325 mesh hafnium carbide powder was accomplished with a hydraulic press and an inductively heated graphite die assembly. The ranges investigated for each variable were as follows: temperature, 3500 to 4870 F; pressure, 1000 to 6030 pounds per square inch; and time, 5 to 60 minutes. Hafnium carbide bodies of approximately 98 percent theoretical density can be produced under the following minimal conditions: 4230 F, 3500 pounds per square inch, and 15 minutes. Further increases in temperature and time resulted only in greater grain size.
Lumber and plywood used in California apartment construction, 1969
George B. Harpole
1973-01-01
The volume of lumber and plywood products used in apartment construction in California was estimated from a sample of apartments for which architectural plans were completed in 1969. Excluding wood mouldings, doors, cabinets, and shelving, an average of 4.85 board feet of lumber and 2.03 square feet (318-inch basis) of plywood per square foot of floor area were used in...
Resonant Acoustic Measurement of Vapor Phase Transport Phenomenon
NASA Astrophysics Data System (ADS)
Schuhmann, R. J.; Garrett, S. L.; Matson, J. V.
2002-12-01
A major impediment to accurate non steady-state diffusion measurements is the ability to accurately measure and track a rapidly changing gas concentration without disturbing the system. Non-destructive methods that do not interfere with system dynamics have been developed in the past. These methods, however, have tended to be cumbersome or inaccurate at low concentrations. A new experimental approach has been developed to measure gaseous diffusion in free air and through porous materials. The method combines the traditional non steady-state laboratory methodology with resonant acoustic gas analysis. A phase-locked-loop (PLL) resonance frequency tracker is combined with a thermally insulated copper resonator. A piston sealed with a metal bellows excites the fundamental standing wave resonance of the resonator. The PLL maintains a constant phase difference (typically 90§) between the accelerometer mounted on the piston and a microphone near the piston to track the resonance frequency in real time. A capillary or glass bead filled core is fitted into an o-ring sealed opening at the end of the resonator opposite the bellows. The rate at which the tracer gas is replaced by air within the resonator is controlled by the diffusion coefficient of the gas in free air through the capillary (DA) or by the effective diffusion coefficient of the gas through the core (De). The mean molecular weight of the gas mixture in the resonator is directly determined six times each minute from the ratio of the absolute temperature to the square of the fundamental acoustic resonance frequency. Average system stability (temperature divided by frequency squared) is better than 350 ppm. DA values for a 0.3-inch diameter capillary were in excellent agreement with published values. De values for porous media samples (0.5 mm glass beads) of four different lengths (1 through 4 inches) using three different tracer gases (He, CH4, Kr) will be reported. Comments will be offered regarding tracer gas selection and device orientation and their effect on experimental results. [Work supported by the Office of Naval Research.
Water for cranberry culture in the Cranmoor area of central Wisconsin
Hamilton, Louis J.
1972-01-01
The Cranmoor area of central Wisconsin is the principal cranberry producing area of the State. Cranberries are grown in only about 2.5 square miles of an 80-square-mile marsh and swamp in the Cranberry Creek basin. Cranberry growers have built reservoirs and ditches throughout 25 square miles of marsh for better management of the area's natural water supply. Additional water is diverted into the basin to supplement the cranberry needs. In the 1966-67 hydrologic budget for Cranberry Creek basin, annual inputs were 27.8 inches of precipitation, 3.8 inches of surface-water diversion into the basin, and 1.1 inches decrease in stored water. Annual outputs were. 20.8 inches of evapotranspiration, 11.7 inches of runoff, and 0.2 inch of groundwater outflow. During the 1966-67 period, precipitation averaged about 3 inches per year below normal. The water used for cranberry culture is almost exclusively surface water. Efficient management of the basin's water supply, plus intermittent diversions of about 100 cubic feet per second from outside the basin, provide cranberry growers with a sufficient quantity of water. Although the quantity of surface water is adequate, the pH (generally 5.7-6.7) is slightly high for optimum use. Dissolved oxygen is slightly low, generally between 4 and 10 milligrams per liter. The water is soft; iron and manganese contents vary seasonally, being high in winter and summer and low in spring. Additional supplies of surface water can be obtained by increasing diversions from outside the basin and by increasing reservoir capacity within the basin. Ground water, although not presently used for cranberries, is available in the central, southern, and eastern parts of the basin, where the thickness of the saturated alluvium exceeds 50 feet. Well yields in these areas might be as much as 1,000 gpm (gallons per minute). Additionally, well yields of as much as 1,000 gpm may be expected from saturated alluvium southeast of Cranberry Creek basin. Where saturated alluvium is less than 50 feet thick, in the northern and western parts of the basin, well yields generally are less than 50 gpm. Ground water is also available from sandstone in the western part of the basin. Where the sandstone is thickest (about 60 ft.), well yields may be as much as 200 gpm. The quality of ground water is similar to that of surface water. The pH of water from the shallow alluvium ranges between 6.0 and 6,6; the pH of water from the deep alluvium is about 7.0. Ground water is soft to moderately hard, 22 to 88 milligrams per liter, and contains excessive amounts of iron and manganese.
Flex-gear electrical power transmission
NASA Technical Reports Server (NTRS)
Vranish, John; Peritt, Jonathan
1993-01-01
This study was conducted to develop an alternative way of transferring electricity across a continuously rotating joint, with little wear and the potential for low electrical noise. The problems with wires, slip rings, electromagnetic couplings, and recently invented roll-rings are discussed. Flex-gears, an improvement of roll-rings, are described. An entire class of flexgear devices is developed. Finally, the preferred flex-gear device is optimized for maximum electrical contact and analyzed for average mechanical power loss and maximum stress. For a device diameter of six inches, the preferred device is predicted to have a total electrical contact area of 0.066 square inches. In the preferred device, a small amount of internal sliding produces a 0.003 inch-pound torque that resists the motion of the device.
Code of Federal Regulations, 2010 CFR
2010-10-01
... that ensure instant release onto a rigidly supported flat horizontal steel plate, which is 2 inches thick and 2 feet square. The plate shall have a clean, dry surface and any microfinish of not less than...
Code of Federal Regulations, 2011 CFR
2011-07-01
...” means gasoline. “Open to the atmosphere” means a compartment that has at least 15 square inches of open area directly exposed to the atmosphere for each cubic foot of net compartment volume. [CGD 76-082, 44...
Code of Federal Regulations, 2013 CFR
2013-07-01
...” means gasoline. “Open to the atmosphere” means a compartment that has at least 15 square inches of open area directly exposed to the atmosphere for each cubic foot of net compartment volume. [CGD 76-082, 44...
Code of Federal Regulations, 2014 CFR
2014-07-01
...” means gasoline. “Open to the atmosphere” means a compartment that has at least 15 square inches of open area directly exposed to the atmosphere for each cubic foot of net compartment volume. [CGD 76-082, 44...
Code of Federal Regulations, 2012 CFR
2012-07-01
...” means gasoline. “Open to the atmosphere” means a compartment that has at least 15 square inches of open area directly exposed to the atmosphere for each cubic foot of net compartment volume. [CGD 76-082, 44...
Code of Federal Regulations, 2010 CFR
2010-07-01
...” means gasoline. “Open to the atmosphere” means a compartment that has at least 15 square inches of open area directly exposed to the atmosphere for each cubic foot of net compartment volume. [CGD 76-082, 44...
NASA Technical Reports Server (NTRS)
Chackerian, Charles, Jr.; Freedman, R.; Giver, L. P.; Brown, L. R.
2001-01-01
The rotationless transition moment squared for the x(sup 1) sigma (sup +) v=3 (left arrow) v=0 band of CO is measured to be the absolute value of R (sub 3-0) squared = 1.7127(25)x 10(exp -7) Debye squared. This value is about 8.6 percent smaller than the value assumed for HITRAN 2000. The Herman-Wallis intensity factor of this band is F=1+0.01168(11)m+0.0001065(79)m squared. The determination of self-broadening coefficients is improved with the inclusion of line narrowing; self-shifts are also reported.
21 CFR 177.1900 - Urea-formaldehyde resins in molded articles.
Code of Federal Regulations, 2010 CFR
2010-04-01
... be mixed with refined wood pulp and the mixture may contain other optional adjuvant substances which... solvent not to exceed 0.5 milligram per square inch of food-contact surface as determined by the methods...
vehicle at 3,000 pounds (lbs.) per square inch and metered on a gasoline gallon equivalent (GGE ); liquefied natural gas (LNG) must be metered on a diesel gallon equivalent (DGE). One GGE of CNG is equal to
21 CFR 175.390 - Zinc-silicon dioxide matrix coatings.
Code of Federal Regulations, 2014 CFR
2014-04-01
... removed by water washing. Iron oxide Lithium hydroxide Removed by water washing. Methyl orange As an acid... § 175.300(c)(3); lithium extractives not to exceed 0.025 milligram per square inch of surface; and...
Hog-ringer speeds seed trap construction
D.O. Hall
1964-01-01
An upholsterer's hog-ringer, with Hill's No. 1 pig rings, increased production of one-foot-square wire seed traps by 25 percent. A design modification allowed two bottom sections to be cut from a 36-inch roll of wire.
40 CFR 280.44 - Methods of release detection for piping.
Code of Federal Regulations, 2012 CFR
2012-07-01
... accordance with the following: (a) Automatic line leak detectors. Methods which alert the operator to the... pounds per square inch line pressure within 1 hour. An annual test of the operation of the leak detector...
40 CFR 280.44 - Methods of release detection for piping.
Code of Federal Regulations, 2011 CFR
2011-07-01
... accordance with the following: (a) Automatic line leak detectors. Methods which alert the operator to the... pounds per square inch line pressure within 1 hour. An annual test of the operation of the leak detector...
40 CFR 280.44 - Methods of release detection for piping.
Code of Federal Regulations, 2013 CFR
2013-07-01
... accordance with the following: (a) Automatic line leak detectors. Methods which alert the operator to the... pounds per square inch line pressure within 1 hour. An annual test of the operation of the leak detector...
40 CFR 280.44 - Methods of release detection for piping.
Code of Federal Regulations, 2014 CFR
2014-07-01
... accordance with the following: (a) Automatic line leak detectors. Methods which alert the operator to the... pounds per square inch line pressure within 1 hour. An annual test of the operation of the leak detector...
40 CFR 280.44 - Methods of release detection for piping.
Code of Federal Regulations, 2010 CFR
2010-07-01
... accordance with the following: (a) Automatic line leak detectors. Methods which alert the operator to the... pounds per square inch line pressure within 1 hour. An annual test of the operation of the leak detector...
Gluability of southern pine earlywood and latewood
Chung Y. Hse
1968-01-01
The gluability and glue-bond durability of southern pine earlywood and latewood were investigated with two-ply, cross-laminated, 1/2-inch-square specimens comprised entirely of earlywood or latewood. A commercial exterior phenolic resin was used.
21 CFR 177.1460 - Melamine-formaldehyde resins in molded articles.
Code of Federal Regulations, 2014 CFR
2014-04-01
... formaldehyde in water solution. (b) The resins may be mixed with refined woodpulp and the mixture may contain... chapter, shall yield net chloroform-soluble extractives not to exceed 0.5 milligram per square inch of...
Apollo 12 stereo view of lunar surface upon which astronaut had stepped
1969-11-20
AS12-57-8448 (19-20 Nov. 1969) --- An Apollo 12 stereo view showing a three-inch square of the lunar surface upon which an astronaut had stepped. Taken during extravehicular activity of astronauts Charles Conrad Jr. and Alan L. Bean, the exposure of the boot imprint was made with an Apollo 35mm stereo close-up camera. The camera was developed to get the highest possible resolution of a small area. The three-inch square is photographed with a flash illumination and at a fixed distance. The camera is mounted on a walking stick, and the astronauts use it by holding it up against the object to be photographed and pulling the trigger. While astronauts Conrad and Bean descended in their Apollo 12 Lunar Module to explore the lunar surface, astronaut Richard F. Gordon Jr. remained with the Command and Service Modules in lunar orbit.
Experimental Investigation of Eccentricity Ratio, Friction, and Oil Flow of Short Journal Bearings
NASA Technical Reports Server (NTRS)
Dubois, G B; Ocvirk, F W
1952-01-01
An experimental investigation was conducted to obtain performance data on bearings of length-diameter ratios of 1, 1/2, and 1/4 for comparison with theoretical curves. A 1.375-inch-diameter bearing was tested at speeds up to 6000 rpm and with unit loads from 0 to 900 pounds per square inch. Experimental data for eccentricity ratio and friction followed single lines when plotted against a theoretically derived capacity number, which is equal to Sommerfeld number times the square of the length-diameter ratio. The form of the capacity number indicates that under certain conditions the eccentricity ratio is theoretically independent of bearing diameter. A method of plotting oil flow data as a single line is shown. Methods are also discussed for approximating a maximum bearing temperature and evaluating the effect of deflection or misalignment on the eccentricity ratio at the ends of the bearings.
RF Sputtering for preparing substantially pure amorphous silicon monohydride
Jeffrey, Frank R.; Shanks, Howard R.
1982-10-12
A process for controlling the dihydride and monohydride bond densities in hydrogenated amorphous silicon produced by reactive rf sputtering of an amorphous silicon target. There is provided a chamber with an amorphous silicon target and a substrate therein with the substrate and the target positioned such that when rf power is applied to the target the substrate is in contact with the sputtering plasma produced thereby. Hydrogen and argon are fed to the chamber and the pressure is reduced in the chamber to a value sufficient to maintain a sputtering plasma therein, and then rf power is applied to the silicon target to provide a power density in the range of from about 7 watts per square inch to about 22 watts per square inch to sputter an amorphous silicon hydride onto the substrate, the dihydride bond density decreasing with an increase in the rf power density. Substantially pure monohydride films may be produced.
Effect of orifice length-diameter ratio on the coefficient of discharge of fuel-injection nozzles
NASA Technical Reports Server (NTRS)
Gelalles, A G; March, E T
1931-01-01
The variation of the coefficient of discharge with the length-diameter ratio of the orifice was determined for nozzles having single orifice 0.008 and 0.020 inch in diameter. Ratios from 0.5 to 10 were investigated at injection pressures from 500 to 5,000 pounds per square inch. The tests showed that, within the error of the observation, the coefficients were the same whether the nozzles were assembled at the end of a constant tube or in an automatic injection valve having a plain stem.
46 CFR 52.01-90 - Materials (modifies PG-5 through PG-13).
Code of Federal Regulations, 2011 CFR
2011-10-01
... subject to stress due to pressure must conform to specifications as indicated in paragraphs PG-5 through...) exceeds 15 pounds per square inch, cross pipes connecting the steam and water drums of water tube boilers...
46 CFR 52.01-90 - Materials (modifies PG-5 through PG-13).
Code of Federal Regulations, 2010 CFR
2010-10-01
... subject to stress due to pressure must conform to specifications as indicated in paragraphs PG-5 through...) exceeds 15 pounds per square inch, cross pipes connecting the steam and water drums of water tube boilers...
Excess flow valve benefit/cost analysis.
DOT National Transportation Integrated Search
1994-12-31
The Office of Pipeline Safety (OPS) is adopting regulations requiring the installation of Excess Flow Valves (EFVs) on all new or renewed single-family residential gas services that operate at pressures that are always 10 psig (pounds per square inch...
40 CFR 65.84 - Operating requirements.
Code of Federal Regulations, 2011 CFR
2011-07-01
...-tight means that the pressure in a truck or railcar tank will not drop more than 750 pascals (0.11 pound per square inch) within 5 minutes after it is pressurized to a minimum of 4,500 pascals (0.65 pound...
50 CFR 261.103 - Basis for determination of a U.S. Standard for Grades.
Code of Federal Regulations, 2012 CFR
2012-10-01
..., fish fillet). (2) Product forms, which describe the types, styles and market forms covered by the...., bruises, blood spots, bones, black spots, coating defects, 1-inch squares, percent by weight, ratios). (8...
50 CFR 261.103 - Basis for determination of a U.S. Standard for Grades.
Code of Federal Regulations, 2010 CFR
2010-10-01
... fillet). (2) Product forms, which describe the types, styles and market forms covered by the standard (e...., bruises, blood spots, bones, black spots, coating defects, 1-inch squares, percent by weight, ratios). (8...
50 CFR 261.103 - Basis for determination of a U.S. Standard for Grades.
Code of Federal Regulations, 2014 CFR
2014-10-01
..., fish fillet). (2) Product forms, which describe the types, styles and market forms covered by the...., bruises, blood spots, bones, black spots, coating defects, 1-inch squares, percent by weight, ratios). (8...
50 CFR 261.103 - Basis for determination of a U.S. Standard for Grades.
Code of Federal Regulations, 2011 CFR
2011-10-01
... fillet). (2) Product forms, which describe the types, styles and market forms covered by the standard (e...., bruises, blood spots, bones, black spots, coating defects, 1-inch squares, percent by weight, ratios). (8...
50 CFR 261.103 - Basis for determination of a U.S. Standard for Grades.
Code of Federal Regulations, 2013 CFR
2013-10-01
..., fish fillet). (2) Product forms, which describe the types, styles and market forms covered by the...., bruises, blood spots, bones, black spots, coating defects, 1-inch squares, percent by weight, ratios). (8...
40 CFR 1051.805 - What symbols, acronyms, and abbreviations does this part use?
Code of Federal Regulations, 2011 CFR
2011-07-01
...—American Society for Testing and Materials. ATV—all-terrain vehicle. cc—cubic centimeters. CFR—Code of...—pounds per square inches of gauge pressure. rpm—revolutions per minute. SAE—Society of Automotive...
Vogel, Karen L.; Reif, Andrew G.
1993-01-01
The 54-square-mile Red Clay Creek Basin, located in the lower Delaware River Basin, is underlain primarily by metamorphic rocks that range from Precambrian to Lower Paleozoic in age. Ground water flows through secondary openings in fractured crystalline rock and through primary openings below the water table in the overlying saprolite. Secondary porosity and permeability vary with hydrogeologic unit, topographic setting, and depth. Thirty-nine percent of the water-bearing zones are encountered within 100 feet of the land surface, and 79 percent are within 200 feet. The fractured crystalline rock and overlying saprolite act as a single aquifer under unconfined conditions. The water table is a subdued replica of the land surface. Local ground-water flow systems predominate in the basin, and natural ground-water discharge is to streams, comprising 62 to 71 percent of streamflow. Water budgets for 1988-90 for the 45-square-mile effective drainage area above the Woodale, Del., streamflow-measurement station show that annual precipitation ranged from 43.59 to 59.14 inches and averaged 49.81 inches, annual streamflow ranged from 15.35 to 26.33 inches and averaged 20.24 inches, and annual evapotranspiration ranged from 27.87 to 30.43 inches and averaged 28.98 inches. The crystalline rocks of the Red Clay Creek Basin were simulated two-dimensionally as a single aquifer under unconfined conditions. The model was calibrated for short-term steady-state conditions on November 2, 1990. Recharge was 8.32 inches per year. Values of aquifer hydraulic conductivity in hillside topographic settings ranged from 0.07 to 2.60 feet per day. Values of streambed hydraulic conductivity ranged from 0.08 to 26.0 feet per day. Prior to simulations where ground-water development was increased, the calibrated steady-state model was modified to approximate long-term average conditions in the basin. Base flow of 11.98 inches per year and a ground-water evapotranspiration rate of 2.17 inches per year were simulated by the model. Different combinations of ground-water supply and wastewater-disposal plans were simulated to assess their effects on the stream-aquifer system. Six of the simulations represent an increase in population of 14,283 and water use of 1.07 million gallons per day. One simulation represents an increase in population of 28,566 and water use of 2.14 million gallons per day. Reduction of average base flow is greatest for development plans with wastewater removed from the basin through sewers and is proportional to the amount of water removed from the basin. The development plan that had the least effect on water levels and base flow included on-lot wells and on-lot septic systems. Five organochlorine insecticides--lindane, DDT, dieldrin, heptachlor, and methoxychlor--were detected in ground water. Four organophosphorus insecticides--malathion, parathion, diazinon, and phorate--were detected in ground water. Four volatile organic compounds--benzene, toluene, tetrachloroethylene, and trichloroethylene--were detected in ground water. Phenol was detected at concentrations up to 8 micrograms per liter in water from 50 percent of 14 wells sampled. The concentration of dissolved nitrate in water from 18 percent of wells sampled exceeded 10 milligrams per liter as nitrogen; concentration of nitrate were as high as 19 milligrams per liter. PCB was detected in the bottom material of West Branch Red Clay Creek at Kennet Square at concentrations up to 5,600 micrograms per kilogram.
Effect of urbanization on the water resources of Warminster Township, Bucks County, Pennsylvania
Sloto, R.A.; Davis, D.K.
1982-01-01
Rapid suburban development occurred in Warminster Township and the surrounding area after World War II, resulting in a large population dependent on ground water. In 1980, approximately 2.7 billion gallons of ground water was pumped by public water suppliers and government facilities. Pumping wells can cause drawdown as far as 2,500 feet undip, downdip, or along strike even if the wells do not penetrate the same strata. Pumping wells have lowered base flow; a stream-gain-and-loss study showed that water lost from Little Neshaminy Creek was about 60 percent of the water pumped from wells near the stream. Net ground-water infiltration to sewers was about 830 million gallons in 1979, a wet year, and about 250 million gallons in 1980, a dry year. Estimated water budgets for 1979 and 1980 indicate evapotranspiration can range from 20 to 26 inches per year (1.0 to 1.2 million gallons per day per square mile) and recharge can range from 8 to 18 inches per year (0.4 to 0.9 million gallons per day per square mile). In a year with average precipitation (45 inches or 2.1 million gallons per day per square mile), evapotranspiration is about 24 inches (1.1 million gallons per day per square mile). Ground-water development in the area influenced by pumping is at its practical limit for years of average recharge, but as much as 1.1 million gallons per day of additional water may be obtained by drilling and pumping wells in areas of Warminster Township not affected by pumping. The concentration of most dissolved constituents increased in water from seven wells, sampled at the onset of urbanization in 1953 and 1956 and again in 1979. Ground-water contamination by volatile organic compounds, especially trichloroethylene and tetrachloroethylene, has made water from some wells unsuitable for public supply. The concentration of lead in 26 samples of ground water ranged from 0 to 55 micrograms per liter, with a median of 17 micrograms per liter; this is above the reported national median and the median in nearby Chester County. High concentrations of sulfate and dissolved solids in ground water are probably caused by restricted gournd-water circulation and may be reduced by long-term pumping, which flushes the aquifer. Effluent from sewage treatment plants has degraded the quality of low streamflow.
Kenneth J. Grayson; Robert F. Wittwer; Michael G. Shelton
2004-01-01
Sixteen shortleaf pine trees were felled in a stand 10 years after an uneven-aged regeneration cut reduced pine basal area to 60 square feet per acre and hardwoods were controlled. Sixteen unreleased trees in an adjacent uncut pine-hardwood stand (120 square feet per acre) were felled for comparison. Sample trees were selected from four 2-inch d.b.h. classes (11, 13,...
A rack-mounted precision waveguide-below-cutoff attenuator with an absolute electronic readout
NASA Technical Reports Server (NTRS)
Cook, C. C.
1974-01-01
A coaxial precision waveguide-below-cutoff attenuator is described which uses an absolute (unambiguous) electronic digital readout of displacement in inches in addition to the usual gear driven mechanical counter-dial readout in decibels. The attenuator is rack-mountable and has the input and output RF connectors in a fixed position. The attenuation rate for 55, 50, and 30 MHz operation is given along with a discussion of sources of errors. In addition, information is included to aid the user in making adjustments on the attenuator should it be damaged or disassembled for any reason.
Effects of irrigation on streamflow in the Central Sand Plain of Wisconsin
Weeks, E.P.; Stangland, H.G.
1971-01-01
Development of ground water for irrigation affects streamflow and water levels in the sand-plain area of central Wisconsin. Additional irrigation development may reduce opportunities for water-based recreation by degrading the streams as trout habitat and by lowering lake levels. This study was made to inventory present development of irrigation in the sand-plain area, assess potential future development, and estimate the effects of irrigation on streamflow and ground-water levels. The suitability of land and the availability of ground water for irrigation are dependent, to a large extent, upon the geology of the area. Rocks making up the ground-water reservoir include outwash, morainal deposits, and glacial lake deposits. These deposits are underlain by crystalline rocks and by sandstone, which act as the floor of the ground-water reservoir. Outwash, the main aquifer, supplies water to about 300 irrigation wells and maintains relatively stable flow in the streams draining the area. The saturated thickness of these deposits is more than 100 feet over much of the area and is as much as 180 feet in bedrock valleys. The saturated thickness of the outwash generally is great enough to provide sufficient water for large-scale irrigation in all but two areas --one near the town of Wisconsin Rapids and one near Dorro Couche Mound. Aquifer tests indicate that the permeability of the outwash is quite high, ranging from about 1,000 gpd per square foot to about 3,800 gpd per square foot, Specific capacities of irrigation wells in the area range from 14 to 157 gpm per foot of drawdown. Water use in the sand-plain area is mainly for irrigation and waterbased recreation. Irrigation development began in the area in the late 1940's, and by 1967 about 19,500 acre-feet of water were pumped to irrigate 34,000 acres of potatoes, snap beans, corn, cucumbers, and other crops. About 70 percent of the applied water was lost to evapotranspiration, and about 30 percent was returned to the ground-water reservoir. Irrigation development should continue in the sand plain; future development probably will include improved artificial drainage and land clearing. The hydrology of the sand-plain area was studied from water budgets for seven basins and from water balances for eight types of vegetative cover or land use. During the study period about 16-20 inches of the 28- to 30-inch average annual precipitation were lost to evapotranspiration from different basins in the area, Evapotranspiration from different types of vegetative cover or land use ranged from about 14 inches per year for bare ground to about 25 inches per year from land covered by phreatophytes. Evapotranspiration is about 19 inches from forested land, about 16 inches from grassland and unirrigated row crops, about 19 inches from irrigated beans, and about 22 inches from irrigated potatoes. Variations in evapotranspiration from the different types of vegetative cover result mainly from differences in soil moisture available to the plants. Available soil moisture ranges from about 1 inch for shallow-rooted grasses and row crops to about 3 inches for forest. Most of the precipitation not used by plants or to replenish soil moisture seeps to the water table, and ground-water recharge in the area averages about 12-14 inches per year. However, computed recharge ranged from about 3 inches to about 22 inches during the 1948-67 period, depending upon the amount and seasonal distribution of precipitation. Of the average 12-14 inches of recharge, about lo-13 inches are discharged to the streams draining the area, and about l-2 inches are used by phreatophytes or by irrigated crops. Annual streamflow in the area averages about 11-12 inches per year, and because it is sustained mainly by ground water, its seasonal distribution is fairly uniform, However, streamflow varies seasonally, being highest in the spring, low in the summer, higher
Federal Register 2010, 2011, 2012, 2013, 2014
2013-07-02
...). Weight: 220-315 grams per square meter. Thread Count (Density): 76-110 ends per inch (Warp) X 70-90 picks.... Finishing Processes: Airjet Dyed. Kim Glas, Chairman Committee for the Implementation of Textile Agreements...
The Tactile Vision Substitution System: Applications in Education and Employment
ERIC Educational Resources Information Center
Scadden, Lawrence A.
1974-01-01
The Tactile Vision Substitution System converts the visual image from a narrow-angle television camera to a tactual image on a 5-inch square, 100-point display of vibrators placed against the abdomen of the blind person. (Author)
Relaxation of Summer Gasoline Volatility Standard for Several Parishes in Louisiana
EPA issued a proposed rule to relax the federal volatility (RVP) standard applicable to gasoline supplied to the 11 Louisiana parishes from 7.8 pounds per square inch (psi) to 9.0 psi during the summer ozone season.
29 CFR 1917.121 - Spiral stairways.
Code of Federal Regulations, 2013 CFR
2013-07-01
... 26.67 cm) in height; (3) Minimum loading capability shall be 100 pounds per square foot (4.79kN), and... shall be a minimum of 11/4 inches (3.18 cm) in outside diameter; and (5) Vertical clearance shall be at...
Potential effects of deep-well waste disposal in western New York
Waller, Roger Milton; Turk, John T.; Dingman, Robert James
1978-01-01
Mathematical and laboratory models were used to observe, respectively, the hydraulic and chemical reactions that may take place during proposed injection of a highly acidic, iron-rich waste pickle liquor into a deep waste-disposal well in western New York. Field temperature and pressure conditions were simulated in the tests. Hydraulic pressure in the middle stages of the initial (1968) injection test had probably hydraulically fractured the Cambrian sandstone-dolomite formation adjacent to the borehole. Transmissivity of the formation is 13 feet squared per day. The proposed rate of injection (72,000 gallons per day) of waste pickle liquor would approach a wellhead pressure of 600 pounds per square inch in about a year. Hydraulic fracturing would reoccur at about 580 pounds per square inch. The measurable cone of influence would extend about 22 miles after injection for 1 year. Chemical reactions between acidic wastes and brine-saturated dolomite would create precipitates that would drastically reduce the permeability of the unfractured part of the dolomite. Nondolomitic sandstone permeability would not be affected by chemical reactions, but the pores might be plugged by the iron-bearing waste. The digital model can be used for qualitative predictions on a regional scale. (Woodard-USGS)
10 CFR 32.55 - Same: Quality assurance; prohibition of transfer.
Code of Federal Regulations, 2010 CFR
2010-01-01
... water for 24 hours and shall show no visible evidence of water entry. Absolute pressure of the air above the water shall then be reduced to 1 inch of mercury. Lowered pressure shall be maintained for 1 minute or until air bubbles cease to be given off by the water, whichever is the longer. Pressure shall...
Annular Internal-External-Expansion Rocket Nozzles for Large Booster Applications
NASA Technical Reports Server (NTRS)
Connors, James F.; Cubbison, Robert W.; Mitchell, Glenn A.
1961-01-01
For large-thrust booster applications, annular rocket nozzles employing both internal and external expansion are investigated. In these nozzles, free-stream air flows through the center as well as around the outside of the exiting jet. Flaps for deflecting the rocket exhaust are incorporated on the external-expansion surface for thrust-vector control. In order to define nozzle off-design performance, thrust vectoring effectiveness, and external stream effects, an experimental investigation was conducted on two annular nozzles with area ratios of 15 and 25 at Mach 0, 2, and 3 in the Lewis 10- by 10-foot wind tunnel. Air, pressurized to 600 pounds per square inch absolute, was used to simulate the exhaust flow. For a nozzle-pressure-ratio range of 40 to 1000, the ratio of actual to ideal thrust was essentially constant at 0.98 for both nozzles. Compared with conventional convergent-divergent configurations on hypothetical boost missions, the performance gains of the annular nozzle could yield significant orbital payload increases (possibly 8 to 17 percent). A single flap on the external-expansion surface of the area-ratio-25 annular nozzle produced a side force equal to 4 percent of the axial force with no measurable loss in axial thrust.
NASA Technical Reports Server (NTRS)
Hastings, E. C., Jr.
1963-01-01
Explorer XVI (1962 Beta Chi l) data that have been analyzed for the period between December 16, 1962 (launch date), and January 13, 1963, indicate that the orbit achieved was close to the predicted orbit. Ten punctures of annealed 0.001-inch-thick beryllium-copper have been used to determine a puncture rate of 0.035 per square foot per day in this material. One puncture of a 0.002-inch-thick sample has also occurred in this period. A tentative evaluation of the puncture rate for the 0.001-inch beryllium-copper in terms of the rate for an equivalent thickness of aluminum has been attempted, and the result has been compared with two different puncture rate estimates. The three micrometeoroid impact detecting systems are operating. Counting rates for the high- and low-sensitivity systems were close to anticipated values near the end of one week. Two of the 0.001-inch-steel-covered grid detectors have been punctured, but none of the 0.003- or 0.006-inch-steel-covered grid detectors have indicated punctures. One of the cadmium sulfide cells indicates three punctures of the 0.00025-inch Mylar cover. None of the 0.002- or 0.003-inch-copper-wire cards have indicated a break in the period covered. Telemetry temperatures were initially higher than expected although they remained well within operating limits. Sensor temperatures have remained within the expected bounds.
16 CFR 1632.4 - Mattress test procedure.
Code of Federal Regulations, 2010 CFR
2010-01-01
... as permanent press or flame resistance. It shall have 120-210 threads per square inch and fabric....4 Commercial Practices CONSUMER PRODUCT SAFETY COMMISSION FLAMMABLE FABRICS ACT REGULATIONS STANDARD... exhausting smoke and/or noxious gases produced by testing. The testroom atmospheric conditions shall be...
46 CFR 169.609 - Exhaust systems.
Code of Federal Regulations, 2013 CFR
2013-10-01
... GUARD, DEPARTMENT OF HOMELAND SECURITY (CONTINUED) NAUTICAL SCHOOLS SAILING SCHOOL VESSELS Machinery and... Machinery” and the following additional requirements: (a) All exhaust installations with pressures in excess of 15 pounds per square inch gage or employing runs passing through living or working spaces must...
46 CFR 169.609 - Exhaust systems.
Code of Federal Regulations, 2012 CFR
2012-10-01
... GUARD, DEPARTMENT OF HOMELAND SECURITY (CONTINUED) NAUTICAL SCHOOLS SAILING SCHOOL VESSELS Machinery and... Machinery” and the following additional requirements: (a) All exhaust installations with pressures in excess of 15 pounds per square inch gage or employing runs passing through living or working spaces must...
Direct Final Rule Approving Relaxation of Summer Gasoline Volatility Standard for Grant Parish Area
EPA is taking direct final action to relax the federal volatility (RVP) standard applicable to summer gasoline supplied to the Grand Parish, Louisiana area from 7.8 pounds per square inch (psi) to 9.0 psi.
Scintillation properties of a 2-inch diameter KCa0.8Sr0.2I3:Eu2+ single crystal
NASA Astrophysics Data System (ADS)
Wu, Yuntao; Lindsey, Adam C.; Loyd, Matthew; Stand, Luis; Zhuravleva, Mariya; Koschan, Merry; Melcher, Charles L.
2017-09-01
Inch-sized scintillating crystals are required for practical radiation detectors such as hand-held radio-isotope identification devices. In this work, a transparent and colorless 2-inch diameter KCa0.8Sr0.2I3: 0 . 5 mo% Eu2+ single crystal was grown by the vertical Bridgman method, and the scintillation properties of a ∅ 50 mm × 45 mm long sample were evaluated. The Eu2+ 5d1- 4 f emission under X-ray excitation is centered at 472 nm. Its scintillation decay time under 137 Cs source irradiation is 2 . 37 μs, and the absolute light output is 51,000 ± 3000 photons/MeV. The energy resolution at 662 keV was evaluated for different orientations of the crystals with respect to the PMT, and the effect of 40 K background subtraction on energy resolution was evaluated. The performance of the packaged crystal was also investigated.
NASA Technical Reports Server (NTRS)
2004-01-01
This mosaic, created from four images taken by the Mars Exploration Rover Opportunity's microscopic imager, outlines the target on 'Bounce' rock that the rover's rock abrasion tool will abrade on sol 66.
This 6-centimeter-square (2.4-inch-square) area was chosen by the rock abrasion tool team as the most advantageous area for grinding. Preliminary results from the rover's miniature thermal emission spectrometer show that Bounce is rich in hematite. Bounce contains spherules, or 'blueberries,' like some rocks in the 'Eagle Crater' outcrop. However, Bounce's spherules appear smaller and may be formed by an entirely different process. The blueberries seen in the outcrop are typically 3 to 4 millimeters (0.12 to 0.16 inch) each. A good example of a cluster of micro-berries can be seen just left of center in this image. Scientists are currently studying all of the rock's features as well as its chemical content. After next sol's grinding operation, the team will be able to compare the rock's exterior and interior chemical compositions.An Experimental Evaluation of Oil Pumping Rings
NASA Technical Reports Server (NTRS)
Eusepi, M. W.; Walowit, J.; Cohen, M.
1981-01-01
The design and construction of a reciprocating test vehicle to be used in evaluating hydrodynamic oil pumping rings are discussed. In addition, experimental test data are presented for three pumping ring designs that were constructed from Tin-Based Babbitt (SAE 11), Bearing Bronze (SAE 660), and Mechanical Carbon Graphite (Union Carbide Grade CNF-J). Data of pumped flow rate versus delivered pressure, as well as friction loss, are reported for the following conditions: frequencies of 10, 35 and 45 Hz; strokes of 25.4 mm (1.00 in.), 38.1 mm (1.50 in.) and 50.8 mm (2.00 in.) oil inlet temperature of 49 degrees (120 degrees); and pumping ring close-in pressures of 10.3 MPa (1500 lb/square inch. A 20W40 automotive oil was used for all tests. The maximum delivered pressure was 11 MPa (1600 lb/square inch. An analysis of hydrodynamic oil pumping rings was performed and the results of the analysis were compared to measured test data.
DOE Office of Scientific and Technical Information (OSTI.GOV)
Meikle, T.; Ballek, L.; Briggs, B.
This study investigates the cost effectiveness of three separate reclamation methods utilized in the long-term establishment of Big Sage (Artemisia tridentata va. wyomingensis). Direct seeding and planting with four cubic inch and ten cubic inch containerized stock were compared using five 36 square meter plots per treatment within a fenced randomized block. Seed plots were hand broadcast at a rate of 2 kilograms per hectare and mulched with certified weed-free wheat straw. Containerized stock plots were planted at a density of one per square meter. Controls with no seeding or planting were established to differentiate actual plant production/reproduction from seedmore » bank recruitment and migration from replaced topsoil and surrounding native areas. Stem density (stem/m{sup 2}), plant height (cm), and plant reproduction (seedlings/m{sup 2}) data will be gathered every spring and fall for three years (1994-1997). Final analysis of the data will relate establishment success to cost efficiency. This initial report on the study reviews only seedling establishment based on first year data.« less
RF sputtering for controlling dihydride and monohydride bond densities in amorphous silicon hydride
Jeffery, F.R.; Shanks, H.R.
1980-08-26
A process is described for controlling the dihydride and monohydride bond densities in hydrogenated amorphous silicone produced by reactive rf sputtering of an amorphous silicon target. There is provided a chamber with an amorphous silicon target and a substrate therein with the substrate and the target positioned such that when rf power is applied to the target the substrate is in contact with the sputtering plasma produced thereby. Hydrogen and argon are fed to the chamber and the pressure is reduced in the chamber to a value sufficient to maintain a sputtering plasma therein, and then rf power is applied to the silicon target to provide a power density in the range of from about 7 watts per square inch to about 22 watts per square inch to sputter an amorphous solicone hydride onto the substrate, the dihydride bond density decreasing with an increase in the rf power density. Substantially pure monohydride films may be produced.
Toward Large-Area Sub-Arcsecond X-Ray Telescopes
NASA Technical Reports Server (NTRS)
ODell, Stephen L.; Aldcroft, Thomas L.; Allured, Ryan; Atkins, Carolyn; Burrows, David N.; Cao, Jian; Chalifoux, Brandon D.; Chan, Kai-Wing; Cotroneo, Vincenzo; Elsner, Ronald F.;
2014-01-01
The future of x-ray astronomy depends upon development of x-ray telescopes with larger aperture areas (approx. = 3 square meters) and fine angular resolution (approx. = 1 inch). Combined with the special requirements of nested grazing-incidence optics, the mass and envelope constraints of space-borne telescopes render such advances technologically and programmatically challenging. Achieving this goal will require precision fabrication, alignment, mounting, and assembly of large areas (approx. = 600 square meters) of lightweight (approx. = 1 kilogram/square meter areal density) high-quality mirrors at an acceptable cost (approx. = 1 million dollars/square meter of mirror surface area). This paper reviews relevant technological and programmatic issues, as well as possible approaches for addressing these issues-including active (in-space adjustable) alignment and figure correction.
A suggestion for computing objective function in model calibration
Wu, Yiping; Liu, Shuguang
2014-01-01
A parameter-optimization process (model calibration) is usually required for numerical model applications, which involves the use of an objective function to determine the model cost (model-data errors). The sum of square errors (SSR) has been widely adopted as the objective function in various optimization procedures. However, ‘square error’ calculation was found to be more sensitive to extreme or high values. Thus, we proposed that the sum of absolute errors (SAR) may be a better option than SSR for model calibration. To test this hypothesis, we used two case studies—a hydrological model calibration and a biogeochemical model calibration—to investigate the behavior of a group of potential objective functions: SSR, SAR, sum of squared relative deviation (SSRD), and sum of absolute relative deviation (SARD). Mathematical evaluation of model performance demonstrates that ‘absolute error’ (SAR and SARD) are superior to ‘square error’ (SSR and SSRD) in calculating objective function for model calibration, and SAR behaved the best (with the least error and highest efficiency). This study suggests that SSR might be overly used in real applications, and SAR may be a reasonable choice in common optimization implementations without emphasizing either high or low values (e.g., modeling for supporting resources management).
30 CFR 7.505 - Structural components.
Code of Federal Regulations, 2011 CFR
2011-07-01
... designed for multiple uses to accommodate the structure's maximum occupancy. (ii) The airlock shall be configured to accommodate a stretcher without compromising its function. (4) Be designed and made to withstand 15 pounds per square inch (psi) overpressure for 0.2 seconds prior to deployment. (5) Be designed...
30 CFR 7.505 - Structural components.
Code of Federal Regulations, 2013 CFR
2013-07-01
... designed for multiple uses to accommodate the structure's maximum occupancy. (ii) The airlock shall be configured to accommodate a stretcher without compromising its function. (4) Be designed and made to withstand 15 pounds per square inch (psi) overpressure for 0.2 seconds prior to deployment. (5) Be designed...
30 CFR 7.505 - Structural components.
Code of Federal Regulations, 2014 CFR
2014-07-01
... designed for multiple uses to accommodate the structure's maximum occupancy. (ii) The airlock shall be configured to accommodate a stretcher without compromising its function. (4) Be designed and made to withstand 15 pounds per square inch (psi) overpressure for 0.2 seconds prior to deployment. (5) Be designed...
30 CFR 7.505 - Structural components.
Code of Federal Regulations, 2012 CFR
2012-07-01
... designed for multiple uses to accommodate the structure's maximum occupancy. (ii) The airlock shall be configured to accommodate a stretcher without compromising its function. (4) Be designed and made to withstand 15 pounds per square inch (psi) overpressure for 0.2 seconds prior to deployment. (5) Be designed...
30 CFR 7.505 - Structural components.
Code of Federal Regulations, 2010 CFR
2010-07-01
... designed for multiple uses to accommodate the structure's maximum occupancy. (ii) The airlock shall be configured to accommodate a stretcher without compromising its function. (4) Be designed and made to withstand 15 pounds per square inch (psi) overpressure for 0.2 seconds prior to deployment. (5) Be designed...
Flat-panel video resolution LED display system
NASA Astrophysics Data System (ADS)
Wareberg, P. G.; Kennedy, D. I.
The system consists of a 128 x 128 element X-Y addressable LED array fabricated from green-emitting gallium phosphide. The LED array is interfaced with a 128 x 128 matrix TV camera. Associated electronics provides for seven levels of grey scale above zero with a grey scale ratio of square root of 2. Picture elements are on 0.008 inch centers resulting in a resolution of 125 lines-per-inch and a display area of approximately 1 sq. in. The LED array concept lends itself to modular construction, permitting assembly of a flat panel screen of any desired size from 1 x 1 inch building blocks without loss of resolution. A wide range of prospective aerospace applications exist extending from helmet-mounted systems involving small dedicated arrays to multimode cockpit displays constructed as modular screens. High-resolution LED arrays are already used as CRT replacements in military film-marking reconnaissance applications.
An investigation of the unsteady flow associated with plume induced flow separation
NASA Technical Reports Server (NTRS)
Boggess, A. L., Jr.
1972-01-01
A wind tunnel study of the basic nature of plume induced flow separation is reported with emphasis on the unsteady aspects of the flow. Testing was conducted in a 6 inch by 6 inch blow-down supersonic wind tunnel. A cone-cylinder model with a pluming jet was used as the test model. Tests were conducted with a systematic variation in Mach number and plume pressure. Results of the tests are presented in the form of root-mean-squared surface pressure levels, power spectral densities, photographs of the flow field from which shock angles and separation lengths were taken, and time-averaged surface pressure profiles.
Artificial Photosynthesis Foundry users, along with staff, have developed a fabrication method to make a square-inch sized artificial photosystem, in the form of an inorganic core-shell nanotube array, that awarded for his pioneering work in the area of advanced x-ray gratings New Catalyst Gives Artificial
21 CFR 177.1030 - Acrylonitrile/butadiene/styrene/methyl methacrylate copolymer.
Code of Federal Regulations, 2011 CFR
2011-04-01
... monomer content of the finished copolymer articles is not more than 11 parts per million as determined by a gas chromatographic method titled “Determination of Residual Acrylonitrile and Styrene Monomers... article shall yield not more than 0.0025 milligram per square inch of acrylonitrile monomer when exposed...
Code of Federal Regulations, 2013 CFR
2013-01-01
... faucet and the flow water pressure in pounds per square inch (psi). [76 FR 12451, Mar. 7, 2011; 76 FR... 10 Energy 3 2013-01-01 2013-01-01 false Faucets. 429.28 Section 429.28 Energy DEPARTMENT OF ENERGY ENERGY CONSERVATION CERTIFICATION, COMPLIANCE, AND ENFORCEMENT FOR CONSUMER PRODUCTS AND COMMERCIAL AND...
Examination of Air Force Crash Damaged or Disabled Aircraft Recovery Program Resourcing
2011-06-01
Positioning for Lift ................................................................................... 2 Figure 4. 26 and 15-Ton Airbags Under Wing...15 Figure 5. Manufacture Depiction of Airbag System...lifting capacities are calculated at an airbag working pressure of seven pounds per square inch. The lifting bag example below is from AGE
The EPA is taking final action to relax the federal volatility (RVP) standard applicable to gasoline supplied to the Birmingham area from 7.8 pounds per square inch (psi) to 9.0 psi during the summer ozone season.
Request from Louisiana to Relax the RVP Standard for Gasoline Sold in Baton Rouge
EPA issued a proposed rule to relax the federal volatility standard applicable to gasoline supplied to the 5 Louisiana parishes of Baton Rouge, Livingston, Ascension, and Iberville from 7.8 pounds per square inch (psi) to 9.0 psi during the summer ozone se
ERIC Educational Resources Information Center
Stifle, Jack
A graphics terminal designed for use as a remote computer input/output terminal is described. Although the terminal is intended for use in teaching applications, it has several features which make it useful in many other computer terminal applications. These features include: a 10-inch square plasma display panel, permanent storage of information…
40 CFR 63.11180 - What definitions do I need to know?
Code of Federal Regulations, 2012 CFR
2012-07-01
... installation, to pavements, or to curbs. Cleaning material means a solvent used to remove contaminants and... portable buildings at the site of installation, to pavements, or to curbs. Facility maintenance also... designed and operated between 0.1 and 10 pounds per square inch gauge (psig) air atomizing pressure...
40 CFR 63.11180 - What definitions do I need to know?
Code of Federal Regulations, 2014 CFR
2014-07-01
... installation, to pavements, or to curbs. Cleaning material means a solvent used to remove contaminants and... portable buildings at the site of installation, to pavements, or to curbs. Facility maintenance also... designed and operated between 0.1 and 10 pounds per square inch gauge (psig) air atomizing pressure...
77 FR 51731 - All-Terrain Vehicle Safety Summit
Federal Register 2010, 2011, 2012, 2013, 2014
2012-08-27
... vehicles (ATVs) are motorized vehicles, designed for off-road use, with three or four broad, low-pressure tires (less than 10 pounds per square inch), a seat designed to be straddled by the operator, and... use restrictions governing issues such as helmet use, riding on pavement, licensing of drivers, and...
40 CFR 63.11180 - What definitions do I need to know?
Code of Federal Regulations, 2011 CFR
2011-07-01
... installation, to pavements, or to curbs. Cleaning material means a solvent used to remove contaminants and... portable buildings at the site of installation, to pavements, or to curbs. Facility maintenance also... designed and operated between 0.1 and 10 pounds per square inch gauge (psig) air atomizing pressure...
40 CFR 63.11180 - What definitions do I need to know?
Code of Federal Regulations, 2010 CFR
2010-07-01
... installation, to pavements, or to curbs. Cleaning material means a solvent used to remove contaminants and... portable buildings at the site of installation, to pavements, or to curbs. Facility maintenance also... designed and operated between 0.1 and 10 pounds per square inch gauge (psig) air atomizing pressure...
40 CFR 63.11180 - What definitions do I need to know?
Code of Federal Regulations, 2013 CFR
2013-07-01
... installation, to pavements, or to curbs. Cleaning material means a solvent used to remove contaminants and... portable buildings at the site of installation, to pavements, or to curbs. Facility maintenance also... designed and operated between 0.1 and 10 pounds per square inch gauge (psig) air atomizing pressure...
L. R. Auchmoody
1976-01-01
A study to determine the reliability of first-year growth measurements obtained from aluminum band dendrometers showed that growth was underestimated for black cherry trees growing less than 0.5 inch in diameter or accumulating less than 0.080 square foot of basal area. Prediction equations to correct for these errors are given.
21 CFR 177.1010 - Acrylic and modified acrylic plastics, semirigid and rigid.
Code of Federal Regulations, 2010 CFR
2010-04-01
... 0.3 milligram per square inch of surface tested. (2) Potassium permanganate oxidizable distilled... permanganate test shall be determined by preparing duplicate permanganate test blanks according to paragraph (c... permanganate test determinations shall be run on samples of distilled water and 8 and 50 percent alcohol...
Interactive Visual Least Absolutes Method: Comparison with the Least Squares and the Median Methods
ERIC Educational Resources Information Center
Kim, Myung-Hoon; Kim, Michelle S.
2016-01-01
A visual regression analysis using the least absolutes method (LAB) was developed, utilizing an interactive approach of visually minimizing the sum of the absolute deviations (SAB) using a bar graph in Excel; the results agree very well with those obtained from nonvisual LAB using a numerical Solver in Excel. These LAB results were compared with…
Water resources of King County, Washington
Richardson, Donald; Bingham, J.W.; Madison, R.J.; Williams, R.
1968-01-01
Although the total supply of water in King County is large, water problems are inevitable because of the large and rapidly expanding population. The county contains a third of the 3 million people in Washington, most of the population being concentrated in the Seattle metropolitan area. King County includes parts of two major physiographic features: the western area is part of the Puget Sound Lowland, and the eastern area is part of the Cascade Range. In these two areas, the terrain, weather, and natural resources (including water) contrast markedly. Average annual precipitation in the county is about 80 inches, ranging from about 30 inches near Puget Sound to more than 150 inches in parts of the Cascades. Annual evapotranspiration is estimated to range from 15 to 24 inches. Average annual runoff ranges from about 15 inches in the lowlands to more than 100 inches in the mountains. Most of the streamflow is in the major basins of the county--the Green-Duwamish, Lake Washington, and Snoqualmie basins. The largest of these is the Snoqualmie River basin (693 square miles), where average annual runoff during the period 1931-60 was about 79 inches. During the same period, annual runoff in the Lake Washington basin ( 607 square miles) averaged about 32 inches, and in the Green-Duwamish River basin (483 square miles), about 46 inches. Seasonal runoff is generally characterized by several high-flow periods in the winter, medium flows in the spring, and sustained low flows in the summer and fall. When floods occur in the county they come almost exclusively between October and March. The threat of flood damage is greatest on the flood plaits of the larger rivers, but in the Green-Duwamish Valley the threat was greatly reduced with the completion of Howard A. Hanson Dam in 1962. In the Snoqualmie River basin, where no such dam exists, the potential damage from a major flood increases each year as additional land is developed in the Snoqualmie Valley. 0nly moderate amounts of sediment are transported by most streams in the county, except during short periods of heavy rain in the winter. The temperature and chemical quality of surface waters are well suited to the requirements of fisheries and for municipal, industrial, and domestic supplies. Little treatment is needed for most uses of surface water, except where the water is subject to pollution. Most recoverable ground water in the county occurs in the Puget Sound Lowland, where great volumes of unconsolidated sedimentary deposits were left by the continental glaciers of the Pleistocene Epoch. Bedrock, most of which is in the Cascade Range, contains very little ground water. Numerous springs, largely undeveloped, occur in several parts of the county. Most of the ground water is of good to excellent quality except for excessive iron, which in some places may require treatment of the water before it is suitable for domestic or industrial use. Excluding water used for hydroelectric-power, recreation, and fisheries, more than 80 percent of the water used in the county is provided by municipal-supply systems. Each of the major river basins includes municipal watersheds that provide large supplies of excellent water. By the 1980's, more than 90 percent of the county's population will probably be served by the Seattle municipal supply. With full development, Seattle's water system would have a capacity sufficient to supply more than 2 million people with 300 gallons per person per day. Most industrial and commercial establishments in the county obtain water from public supply systems. The most .serious water problem in the county at present (1965) is the threat of pollution in the densely populated areas. The immediate threat in the Seattle area is being reduced by the sewage-treatment program of the Municipality of Metropolitan Seattle, which will eliminate the discharge of waste into Lake Washington. Expected increases in population and industry will introd
DOE Office of Scientific and Technical Information (OSTI.GOV)
Stredde, H.; /Fermilab
1998-05-27
A lifting fixture has been designed to handle the Samus counters. These counters are being removed from the D-zero area and will be transported off site for further use at another facility. This fixture is designed specifically for this particular application and will be transferred along with the counters. The future use of these counters may entail installation at a facility without access to a crane and therefore a lift fixture suitable for both crane and/or fork lift usage has been created The counters weigh approximately 3000 lbs. and have threaded rods extended through the counter at the top comersmore » for lifting. When these counters were first handled/installed these rods were used in conjunction with appropriate slings and handled by crane. The rods are secured with nuts tightened against the face of the counter. The rod thread is M16 x 2({approx}.625-inch dia.) and extends 2-inch (on average) from the face of the counter. It is this cantilevered rod that the lift fixture engages with 'C' style plates at the four top comers. The strongback portion of the lift fixture is a steel rectangular tube 8-inch (vertical) x 4-inch x .25-inch wall, 130-inch long. 1.5-inch square bars are welded perpendicular to the long axis of the rectangular tube at the appropriate lift points and the 'C' plates are fastened to these bars with 3/4-10 high strength bolts -grade 8. Two short channel sections are positioned-welded-to the bottom of the rectangular tube on 40 feet centers, which are used as locators for fork lift tines. On the top are lifting eyes for sling/crane usage and are rated at 3500 lbs. safe working load each - vertical lift only.« less
Process to restore obliterated serial numbers on metal surfaces
NASA Technical Reports Server (NTRS)
Young, S. G.; Parker, B.; Chisum, W. J.
1974-01-01
Metal smeared into grooves of serial numbers by grinding or filing can be cleaned out by process called cavitation. Ultrasonic vibrator generates very high frequency vibrations in water which create millions of microscopic bubbles. Cavitation bubbles impact metal surface at thousands of pounds per square inch pressure. Metal particles filling grooves are broken away.
46 CFR 56.97-40 - Installation tests.
Code of Federal Regulations, 2011 CFR
2011-10-01
...) and 56.50-40(b), respectively. (2) Fuel oil discharge piping between the pumps and the burners, but.... (5) Any Class I, I-L, II-L piping. (6) Cargo oil piping. (7) Firemains, but not less than 150 pounds per square inch. (8) Fuel oil transfer and filling piping. (9) Class I compressed air piping. (10...
30 CFR 18.31 - Enclosures-joints and fastenings.
Code of Federal Regulations, 2011 CFR
2011-07-01
... square inch (gage). Castings shall be free from blowholes. (2) Welded joints forming an enclosure shall... portion are acceptable in lieu of a head or shoulder, but cotter pins and similar devices shall not be... attaching hose conduit, unless energy carried by the cable is intrinsically safe. (c) No assembly will be...
30 CFR 18.31 - Enclosures-joints and fastenings.
Code of Federal Regulations, 2012 CFR
2012-07-01
... square inch (gage). Castings shall be free from blowholes. (2) Welded joints forming an enclosure shall... portion are acceptable in lieu of a head or shoulder, but cotter pins and similar devices shall not be... attaching hose conduit, unless energy carried by the cable is intrinsically safe. (c) No assembly will be...
30 CFR 18.31 - Enclosures-joints and fastenings.
Code of Federal Regulations, 2013 CFR
2013-07-01
... square inch (gage). Castings shall be free from blowholes. (2) Welded joints forming an enclosure shall... portion are acceptable in lieu of a head or shoulder, but cotter pins and similar devices shall not be... attaching hose conduit, unless energy carried by the cable is intrinsically safe. (c) No assembly will be...
40 CFR 1051.805 - What symbols, acronyms, and abbreviations does this part use?
Code of Federal Regulations, 2012 CFR
2012-07-01
...—American Society for Testing and Materials. ATV—all-terrain vehicle. cc—cubic centimeters. CFR—Code of...—pounds per square inches of gauge pressure. rpm—revolutions per minute. SAE—Society of Automotive Engineers. SI—spark-ignition. THC—total hydrocarbon. THCE—total hydrocarbon equivalent. U.S.C.—United States...
40 CFR 1051.805 - What symbols, acronyms, and abbreviations does this part use?
Code of Federal Regulations, 2014 CFR
2014-07-01
...—American Society for Testing and Materials. ATV—all-terrain vehicle. cc—cubic centimeters. CFR—Code of...—pounds per square inches of gauge pressure. rpm—revolutions per minute. SAE—Society of Automotive Engineers. SI—spark-ignition. THC—total hydrocarbon. THCE—total hydrocarbon equivalent. U.S.C.—United States...
40 CFR 1051.805 - What symbols, acronyms, and abbreviations does this part use?
Code of Federal Regulations, 2013 CFR
2013-07-01
...—American Society for Testing and Materials. ATV—all-terrain vehicle. cc—cubic centimeters. CFR—Code of...—pounds per square inches of gauge pressure. rpm—revolutions per minute. SAE—Society of Automotive Engineers. SI—spark-ignition. THC—total hydrocarbon. THCE—total hydrocarbon equivalent. U.S.C.—United States...
46 CFR 31.10-18 - Firefighting equipment: General-TB/ALL.
Code of Federal Regulations, 2013 CFR
2013-10-01
... extinguishing agent is needed. Carbon dioxide Weigh cylinders. Recharge if weight loss exceeds 10 percent of... ascertain that the system is in good operating condition. For carbon dioxide or clean agent systems as... be tested with at least 50 pounds per square inch of air pressure or by blowing steam through the...
46 CFR 31.10-18 - Firefighting equipment: General-TB/ALL.
Code of Federal Regulations, 2014 CFR
2014-10-01
... extinguishing agent is needed. Carbon dioxide Weigh cylinders. Recharge if weight loss exceeds 10 percent of... ascertain that the system is in good operating condition. For carbon dioxide or clean agent systems as... be tested with at least 50 pounds per square inch of air pressure or by blowing steam through the...
49 CFR 230.25 - Maximum allowable stress on stays and braces.
Code of Federal Regulations, 2010 CFR
2010-10-01
... 49 Transportation 4 2010-10-01 2010-10-01 false Maximum allowable stress on stays and braces. 230... Boilers and Appurtenances Allowable Stress § 230.25 Maximum allowable stress on stays and braces. The maximum allowable stress per square inch of net cross sectional area on fire box and combustion chamber...
Code of Federal Regulations, 2014 CFR
2014-01-01
... faucets, the maximum water use in gallons per cycle (gal/cycle) rounded to the nearest 0.01 gallon; and for all faucet types, the flow water pressure in pounds per square inch (psi). [76 FR 12451, Mar. 7... 10 Energy 3 2014-01-01 2014-01-01 false Faucets. 429.28 Section 429.28 Energy DEPARTMENT OF ENERGY...
49 CFR 571.108 - Standard No. 108; Lamps, reflective devices, and associated equipment.
Code of Federal Regulations, 2011 CFR
2011-10-01
... square inches). (2) Shall meet the visibility requirements specified in S5.3.2(c). (3) Shall have the... Transmittance of Transparent Plastic; (c) After the outdoor exposure test, plastic materials used for reflex... no change in shape and general appearance discernable to the naked eye when compared with an...
16 CFR 1632.4 - Mattress test procedure.
Code of Federal Regulations, 2014 CFR
2014-01-01
... directly over the thread or in the depression created by the quilting process on the half of the test... characteristic such as permanent press or flame resistance. It shall have 120-210 threads per square inch and... their full lengths over the thread or depression, then the cigarettes shall be positioned in a manner...
16 CFR 1632.4 - Mattress test procedure.
Code of Federal Regulations, 2011 CFR
2011-01-01
... directly over the thread or in the depression created by the quilting process on the half of the test... as permanent press or flame resistance. It shall have 120-210 threads per square inch and fabric... their full lengths over the thread or depression, then the cigarettes shall be positioned in a manner...
40 CFR 180.1189 - Methyl salicylate; exemption from the requirement of a tolerance.
Code of Federal Regulations, 2011 CFR
2011-07-01
... food or feed when used as an insect repellant in food packaging and animal feed packaging at an application rate that does not exceed 0.2 mg of methyl salicylate per square inch of packaging materials. [62... AGENCY (CONTINUED) PESTICIDE PROGRAMS TOLERANCES AND EXEMPTIONS FOR PESTICIDE CHEMICAL RESIDUES IN FOOD...
40 CFR 180.1189 - Methyl salicylate; exemption from the requirement of a tolerance.
Code of Federal Regulations, 2010 CFR
2010-07-01
... food or feed when used as an insect repellant in food packaging and animal feed packaging at an application rate that does not exceed 0.2 mg of methyl salicylate per square inch of packaging materials. [62... AGENCY (CONTINUED) PESTICIDE PROGRAMS TOLERANCES AND EXEMPTIONS FOR PESTICIDE CHEMICAL RESIDUES IN FOOD...
Federal Register 2010, 2011, 2012, 2013, 2014
2011-05-02
... Activities; Submission to OMB for Review and Approval; Comment Request; Fuels and Fuel Additives: Gasoline...: Regulation of Fuels and Fuel Additives: Gasoline Volatility (Renewal). ICR numbers: EPA ICR No. 1367.09, OMB...: Gasoline volatility, as measured by Reid Vapor Pressure (RVP) in pounds per square inch (psi), is...
40 CFR 1051.805 - What symbols, acronyms, and abbreviations does this part use?
Code of Federal Regulations, 2010 CFR
2010-07-01
... Definitions and Other Reference Information § 1051.805 What symbols, acronyms, and abbreviations does this...—American Society for Testing and Materials. ATV—all-terrain vehicle. cc—cubic centimeters. CFR—Code of...—pounds per square inches of gauge pressure. rpm—revolutions per minute. SAE—Society of Automotive...
46 CFR 72.05-25 - Doors, other than watertight.
Code of Federal Regulations, 2011 CFR
2011-10-01
... glass shall be fitted in steel or equivalent metal frames and shall be retained by steel or equivalent metal glazing beads or angles. (5) Where wire-inserted glass is required, and the single wire type is.... The cut for the hose port should be approximately 6 inches square. A hinged or pivoted steel or...
46 CFR 72.05-25 - Doors, other than watertight.
Code of Federal Regulations, 2010 CFR
2010-10-01
... glass shall be fitted in steel or equivalent metal frames and shall be retained by steel or equivalent metal glazing beads or angles. (5) Where wire-inserted glass is required, and the single wire type is.... The cut for the hose port should be approximately 6 inches square. A hinged or pivoted steel or...
49 CFR 393.43 - Breakaway and emergency braking.
Code of Federal Regulations, 2012 CFR
2012-10-01
... independent of brake air, hydraulic, and other pressure, and independent of other controls, unless the braking... protection valve or similar device shall operate automatically when the air pressure on the towing vehicle is... to a fixed pressure which shall not be lower than 20 pounds per square inch nor higher than 45 pounds...
49 CFR 393.43 - Breakaway and emergency braking.
Code of Federal Regulations, 2013 CFR
2013-10-01
... independent of brake air, hydraulic, and other pressure, and independent of other controls, unless the braking... protection valve or similar device shall operate automatically when the air pressure on the towing vehicle is... to a fixed pressure which shall not be lower than 20 pounds per square inch nor higher than 45 pounds...
49 CFR 393.43 - Breakaway and emergency braking.
Code of Federal Regulations, 2014 CFR
2014-10-01
... independent of brake air, hydraulic, and other pressure, and independent of other controls, unless the braking... protection valve or similar device shall operate automatically when the air pressure on the towing vehicle is... to a fixed pressure which shall not be lower than 20 pounds per square inch nor higher than 45 pounds...
30 CFR 75.1100-1 - Type and quality of firefighting equipment.
Code of Federal Regulations, 2013 CFR
2013-07-01
... extinguishing capacity equivalent to that of a portable water car. (d) Portable foam-generating machines or devices: A portable foam-generating machine or device shall have facilities and equipment for supplying the machine with 30 gallons of water per minute at 30 pounds per square inch for a period of 35...
30 CFR 75.1100-1 - Type and quality of firefighting equipment.
Code of Federal Regulations, 2014 CFR
2014-07-01
... extinguishing capacity equivalent to that of a portable water car. (d) Portable foam-generating machines or devices: A portable foam-generating machine or device shall have facilities and equipment for supplying the machine with 30 gallons of water per minute at 30 pounds per square inch for a period of 35...
40 CFR 180.1189 - Methyl salicylate; exemption from the requirement of a tolerance.
Code of Federal Regulations, 2012 CFR
2012-07-01
... food or feed when used as an insect repellant in food packaging and animal feed packaging at an application rate that does not exceed 0.2 mg of methyl salicylate per square inch of packaging materials. [62... AGENCY (CONTINUED) PESTICIDE PROGRAMS TOLERANCES AND EXEMPTIONS FOR PESTICIDE CHEMICAL RESIDUES IN FOOD...
40 CFR 180.1189 - Methyl salicylate; exemption from the requirement of a tolerance.
Code of Federal Regulations, 2014 CFR
2014-07-01
... food or feed when used as an insect repellant in food packaging and animal feed packaging at an application rate that does not exceed 0.2 mg of methyl salicylate per square inch of packaging materials. [62... AGENCY (CONTINUED) PESTICIDE PROGRAMS TOLERANCES AND EXEMPTIONS FOR PESTICIDE CHEMICAL RESIDUES IN FOOD...
40 CFR 180.1189 - Methyl salicylate; exemption from the requirement of a tolerance.
Code of Federal Regulations, 2013 CFR
2013-07-01
... food or feed when used as an insect repellant in food packaging and animal feed packaging at an application rate that does not exceed 0.2 mg of methyl salicylate per square inch of packaging materials. [62... AGENCY (CONTINUED) PESTICIDE PROGRAMS TOLERANCES AND EXEMPTIONS FOR PESTICIDE CHEMICAL RESIDUES IN FOOD...
40 CFR 65.84 - Operating requirements.
Code of Federal Regulations, 2010 CFR
2010-07-01
...) CONSOLIDATED FEDERAL AIR RULE Transfer Racks § 65.84 Operating requirements. (a) Closed vent systems or process piping. An owner or operator of a transfer rack shall operate it in such a manner that emissions are... per square inch). (d) Pressure relief device. The owner or operator of a transfer rack subject to the...
21 CFR 178.3860 - Release agents.
Code of Federal Regulations, 2014 CFR
2014-04-01
... centimeter (1.29 milligrams per square inch) of backing. Rice bran wax For use only in plastics intended for... 21 Food and Drugs 3 2014-04-01 2014-04-01 false Release agents. 178.3860 Section 178.3860 Food and Drugs FOOD AND DRUG ADMINISTRATION, DEPARTMENT OF HEALTH AND HUMAN SERVICES (CONTINUED) INDIRECT FOOD...
Estimating 1970-99 average annual groundwater recharge in Wisconsin using streamflow data
Gebert, Warren A.; Walker, John F.; Kennedy, James L.
2011-01-01
Average annual recharge in Wisconsin for the period 1970-99 was estimated using streamflow data from U.S. Geological Survey continuous-record streamflow-gaging stations and partial-record sites. Partial-record sites have discharge measurements collected during low-flow conditions. The average annual base flow of a stream divided by the drainage area is a good approximation of the recharge rate; therefore, once average annual base flow is determined recharge can be calculated. Estimates of recharge for nearly 72 percent of the surface area of the State are provided. The results illustrate substantial spatial variability of recharge across the State, ranging from less than 1 inch to more than 12 inches per year. The average basin size for partial-record sites (50 square miles) was less than the average basin size for the gaging stations (305 square miles). Including results for smaller basins reveals a spatial variability that otherwise would be smoothed out using only estimates for larger basins. An error analysis indicates that the techniques used provide base flow estimates with standard errors ranging from 5.4 to 14 percent.
Water-Pressure Distribution on Seaplane Float
NASA Technical Reports Server (NTRS)
Thompson, F L
1929-01-01
The investigation presented in this report was conducted for the purpose of determining the distribution and magnitude of water pressures likely to be experienced on seaplane hulls in service. It consisted of the development and construction of apparatus for recording water pressures lasting one one-hundredth second or longer and of flight tests to determine the water pressures on a UO-1 seaplane float under various conditions of taxiing, taking off, and landing. The apparatus developed was found to operate with satisfactory accuracy and is suitable for flight tests on other seaplanes. The tests on the UO-1 showed that maximum pressures of about 6.5 pounds per square inch occur at the step for the full width of the float bottom. Proceeding forward from the step the maximum pressures decrease in magnitude uniformly toward the bow, and the region of highest pressures narrows toward the keel. Immediately abaft the step the maximum pressures are very small, but increase in magnitude toward the stern and there once reached a value of about 5 pounds per square inch. (author)
Water resources of Kosrae, Caroline Islands
Van der Brug, Otto
1984-01-01
Kosrae is a high volcanic island about 42 square miles in area and the easternmost of the Caroline Islands. Mount Finkol (Mt. Crozer), at 2,065 feet, is the highest point on the island. Mountainous ridges descend sharply to narrow coastal strips which support a population of 5,500 people. Many streams, some quite large relative to the size of the island, drain radially from the interior. The average annual discharge of surface water amounts to almost 7 million gallons per square mile per day. Annual rainfall for coastal areas on Kosrae averages about 200 inches, and is similar to the rainfall for coastal areas on the island of Ponape, about 340 statute miles to the northwest. Rainfall in the interior was estimated at 225 inches per year of which about two thirds runs off as streamflow. Surface-water quality is very good as shown by 42 chemical analyses of water from 12 streams. This report summarizes in one volume the hydrologic data collected and provides interpretations that can be used by planning and public works officials as a basis for making decisions on the development and management of their water resources. (USGS)
Cummans, J.E.
1976-01-01
Low-flow-frequency data are tabulated for 90 streamflow sites on the Kitsap Peninsula and adjacent islands, Washington. Also listed are data for 56 additional sites which have insufficient measurements for frequency analysis but which have been observed having no flow at least once during the low-flow period. The streams drain relatively small basins; only three streams have drainage areas greater than 20.0 square miles, and only nine other streams have drainage areas greater than 10.0 square miles. Mean annual precipitation during the period 1931-60 ranged from about 25 inches near Hansville to about 70 inches near Tahuya. Low-flow-frequency curves plotted from records of streamflow at eight long-term gaging stations were used to determine data for low-flow durations of 7, 30, 60, 90, and 183 days. Regression techniques then were used to estimate low flows with frequencies up to 20 years for stations with less than 10 years of record and for miscellaneous sites where discharge measurements have been made. (Woodard-USGS)
2002-03-13
NASA's Marshall Space Flight Center (MSFC) in Huntsville, Alabama, has begun a series of engine tests on the Reaction Control Engine developed by TRW Space and Electronics for NASA's Space Launch Initiative (SLI). SLI is a technology development effort aimed at improving the safety, reliability, and cost effectiveness of space travel for reusable launch vehicles. The engine in this photo, the first engine tested at MSFC that includes SLI technology, was tested for two seconds at a chamber pressure of 185 pounds per square inch absolute (psia). Propellants used were liquid oxygen as an oxidizer and liquid hydrogen as fuel. Designed to maneuver vehicles in orbit, the engine is used as an auxiliary propulsion system for docking, reentry, fine-pointing, and orbit transfer while the vehicle is in orbit. The Reaction Control Engine has two unique features. It uses nontoxic chemicals as propellants, which creates a safer environment with less maintenance and quicker turnaround time between missions, and it operates in dual thrust modes, combining two engine functions into one engine. The engine operates at both 25 and 1,000 pounds of force, reducing overall propulsion weight and allowing vehicles to easily maneuver in space. The force of low level thrust allows the vehicle to fine-point maneuver and dock, while the force of the high level thrust is used for reentry, orbital transfer, and course positioning.
Low Emission Hydrogen Combustors for Gas Turbines Using Lean Direct Injection
NASA Technical Reports Server (NTRS)
Marek, C. John; Smith, Timothy D.; Kundu, Krishna
2005-01-01
One of the key technology challenges for the use of hydrogen in gas turbine engines is the performance of the combustion system, in particular the fuel injectors. To investigate the combustion performance of gaseous hydrogen fuel injectors flame tube combustor experiments were performed. Tests were conducted to measure the nitrogen oxide (NOx) emissions and combustion performance at inlet conditions of 600 to 1000 deg F, 60 to 200 pounds per square inch absolute (psia), and equivalence ratios up to 0.48. All the injectors were based on Lean Direct Injection (LDI) technology with multiple injection points and quick mixing. One challenge to hydrogen based premixing combustion systems is flashback since hydrogen has a reaction rate over seven times that of Jet-A. To reduce the risk, design mixing times were kept short and velocities high to minimize flashback. Five fuel injector designs were tested in 2.5 and 3.5-in. diameter flame tubes with non-vitiated heated air and gaseous hydrogen. Data is presented on measurements of NOx emissions and combustion efficiency for the hydrogen injectors at 1.0, 3.125, and 5.375 in. from the injector face. Results show that for some configurations, NOx emissions are comparable to that of state of the art Jet-A LDI combustor concepts.
Yield of pallet cants and lumber from hardwood poletimber thinnings
E. Paul Craft; David M. Emanuel
1981-01-01
Woods-run bolts in 4- and 6-foot length from poletimber stand thininings were classified into five quality classes, and the absolute sweep was measured for each bolt. Cants 4 by 4 and 4 by 6 inches were sawn from these bolts. The cants were classified by an interim classification system for the production of pallet parts. In contrast to straight bolts, sweep from 0.6...
Floods of November-December 1950 in western Nevada
Wells, J.V.B.
1954-01-01
Record-breaking floods in the Walker, Carson, and Truckee River basins during November and December 1950 resulted from a rapid sequence of storms and unseasonably high temperatures that melted most of the early snow cover. During the period November 13 to December 8, 1950, total precipitation ranged from about 5 inches at the foot of the Sierra Nevada in Nevada to about 30 inches at the crest in California, near the California-Nevada State line. About half of this total occurred during the period November 16-21. The resulting floods were the greatest in more than 50 years of record. The highest discharge occurred on Truckee River where the greatest damage potential exists?in the urban area of Reno and Sparks. Notable rates of discharge were 19,900 cfs, or 36.1 cfs per square mile, from 551 square miles in Truckee River at Reno, Nev.; 7,010 cfs, or 212 cfs per square mile, from 33 square miles in Little Truckee River near Hobart Mills, Calif.; and 3,570 cfs, or 119 cfs per square mile, from 30 square miles in East Fork Carson River near Markleeville, Calif. The estimate of damages compiled by the Corps of Engineers total $4,360,000 for the area; $1,982,000 of this was for Reno. Two deaths were reported. The American Red Cross assisted about 200 persons, at an expenditure of about $7,500. Federal aid for city and county rehabilitation in Nevada totaled $75,000. This report contains records of stage and discharge at 20 gaging stations and contents of 2 reservoirs, and a summary of peak discharges at 23 points within or adjacent to the flood area. The report contains also a discussion of the storms and floods, a section on meteorology prepared by the Weather Bureau, and a brief discussion of previous floods.
An Aerial Radiological Survey of the City of North Las Vegas (Downtown) and the Motor Speedway
DOE Office of Scientific and Technical Information (OSTI.GOV)
Piotr Wasiolek
2007-12-01
As part of the proficiency training for the Radiological Mapping mission of the Aerial Measuring System (AMS), a survey team from the Remote Sensing Laboratory-Nellis (RSL-Nellis) conducted an aerial radiological survey on December 11-12, 2007, with the purpose of mapping natural radiation background and locating any man-made radioactive sources. The survey covered 19.4 square miles (9.2 square miles over the downtown area of the City of North Las Vegas and 10.2 square miles over the Las Vegas Motor Speedway [LVMS]). The flight lines over the surveyed areas are presented in Figures 1 and 2. A total of four 2.5-hour-long flightsmore » were performed at an altitude of 150 ft above ground level (AGL) with 300 ft of flight line spacing. Water line and test line flights were conducted over the Lake Mead and Government Wash areas to ensure quality control of the data. The data were collected by the AMS data acquisition system-REDAR V using an array of twelve 2-inch x 4-inch x 16-inch sodium iodide (NaI) detectors flown on-board a twin-engine Bell 412 helicopter. Data in the form of gamma energy spectra were collected continually (every second) over the course of the survey and were geo-referenced using a differential Global Positioning System. Collection of spectral data allows the system to distinguish between ordinary fluctuations in natural background radiation levels and the signature produced by man-made radioisotopes sources. Spectral data can also be used to identify specific radioactive isotopes. As a courtesy service with the approval of the U.S. Department of Energy, National Nuclear Security Administration, Nevada Site Office, RSL-Nellis is providing this summary to the office of the Mayor of City of North Las Vegas and LVMS security along with the gross counts-based exposure rate and man-made counts maps.« less
Feasibility study of solid surface subreflector production techniques
NASA Technical Reports Server (NTRS)
1982-01-01
The principal effort was to study technical feasibility and cost aspects of the production technique of spin forming a subreflector reflective surface to a desired surface of revolution, back the surface with fiberglass to stabilize it sufficiently so that it may be machined to the target surface tolerance of .008 inches Root Mean Square (RMS) with a goal of .003 inches RMS. To verify this production technique, analyses was performed to define the production procedure. A price estimate for a 150 inch diameter subreflector for a 34 meter cassegrain antenna. During this feasibility study, numerous production processes were evaluated theoretically as production approaches for single surface, non-welded subreflectors. The first successful was the principal process of spin forming the reflective surface, backing with fiberglass and machining to a final contour. The second successful process was spin forming or bump forming a thicker reflective surface, with an integral (welded in) structure as a backing and machining the mounting pads and reflector to a final configuration.
Effect of Moderate Air Flow on the Distribution of Fuel Sprays After Injection Cut-0ff
NASA Technical Reports Server (NTRS)
Rothrock, A M; Spencer, R C
1935-01-01
High-speed motion pictures were taken of fuel sprays with the NACA spray-photographic apparatus to study the distribution of the liquid fuel from the instant of injection cut-off until about 0.05 second later. The fuel was injected into a glass-walled chamber in which the air density was varied from 1 to 13 times atmospheric air density (0.0765 to 0.99 pound per cubic foot) and in which the air was at room temperature. The air in the chamber was set in motion by means of a fan, and was directed counter to the spray at velocities up to 27 feet per second. The injection pressure was varied from 2,000 to 6,000 pounds per square inch. A 0.20-inch single-orifice nozzle, an 0.008-inch single-orifice nozzle, a multiorifice nozzle, and an impinging-jets nozzle were used. The best distribution was obtained by the use of air and a high-dispersion nozzle.
29 CFR 1917.121 - Spiral stairways.
Code of Federal Regulations, 2010 CFR
2010-07-01
... minimum dimensions of Figure F-1; EC21OC91.020 Spiral Stairway—Minimum Dimensions A (half-tread width) B... 26.67 cm) in height; (3) Minimum loading capability shall be 100 pounds per square foot (4.79kN), and... least 6 feet, 6 inches (1.98 m) above the top step. (c) Maintenance. Spiral stairways shall be...
29 CFR 1917.121 - Spiral stairways.
Code of Federal Regulations, 2011 CFR
2011-07-01
... minimum dimensions of Figure F-1; EC21OC91.020 Spiral Stairway—Minimum Dimensions A (half-tread width) B... 26.67 cm) in height; (3) Minimum loading capability shall be 100 pounds per square foot (4.79kN), and... least 6 feet, 6 inches (1.98 m) above the top step. (c) Maintenance. Spiral stairways shall be...
Federal Register 2010, 2011, 2012, 2013, 2014
2011-07-08
... ENVIRONMENTAL PROTECTION AGENCY 40 CFR Part 52 [EPA-R05-OAR-2006-0976; FRL-9430-5] Approval and Promulgation of Air Quality Implementation Plans; Ohio; Control of Gasoline Volatility; Correction AGENCY... a gasoline Reid Vapor Pressure (RVP) limit of 7.8 pounds per square inch (psi) for gasoline sold in...
7 CFR 51.613 - Serious damage.
Code of Federal Regulations, 2014 CFR
2014-01-01
... aggregating more than one square inch on the midrib portion of the branch or branches. (c) Growth cracks, when the stalk has more than two branches affected by growth cracks any of which are more than one-half... fifteen hair-like lines of any length on one or more heart branches, or when there are more than one and...
7 CFR 51.613 - Serious damage.
Code of Federal Regulations, 2013 CFR
2013-01-01
... aggregating more than one square inch on the midrib portion of the branch or branches. (c) Growth cracks, when the stalk has more than two branches affected by growth cracks any of which are more than one-half... fifteen hair-like lines of any length on one or more heart branches, or when there are more than one and...
Matchmaker, Matchmaker, Find Me a Roommate
ERIC Educational Resources Information Center
Lipka, Sara
2008-01-01
Blind dates can go awry, but a roommate mismatch can spoil a semester. Nasty habits. Bitter grudges. Epic stand-offs over square inches. Luckily, most pairings don't get that ugly, whether campuses make them randomly or by running survey responses through a computer. These days many students even control their own fates: More and more colleges let…
Density and Age Affect Performance of Containerized Loblolly Pine Seedlings
James P. Barnett
1980-01-01
Loblolly pine seedlings were grown in 1 x 5 inch biodegradable plastic tubes for 10, 12, and 14 weeks at densities of 42, 84, 126, and 168 per square foot. Seedling density and age significantly affected seedling development at time of outplanting, and density became more important as greenhouse growing times increased. All morphological characteristics measured when...
Instrument for the measurement and determination of chemical pulse column parameters
Marchant, Norman J.; Morgan, John P.
1990-01-01
An instrument for monitoring and measuring pneumatic driving force pulse parameters applied to chemical separation pulse columns obtains real time pulse frequency and root mean square amplitude values, calculates column inch values and compares these values against preset limits to alert column operators to the variations of pulse column operational parameters beyond desired limits.
49 CFR 232.403 - Design standards for one-way end-of-train devices.
Code of Federal Regulations, 2010 CFR
2010-10-01
... valve to prevent explosion from a high pressure air leak inside the rear unit. (c) Reporting rate... shall be capable of determining the brake pipe pressure on the rear car and transmitting that... measuring the brake pipe pressure on the rear car with an accuracy of ±3 pounds per square inch (psig) and...
Code of Federal Regulations, 2013 CFR
2013-10-01
... Special Use Hunting Permit, which hunters must sign and carry on their person while hunting. 4. The hunt... than 6 p.m. 6. Hunters must sign in and out on each hunt day. 7. We prohibit use of dogs. 8. We.... Scouts must wear 400 square inches (2,600 cm2) of visible blaze orange. We require hunters to sign in and...
Code of Federal Regulations, 2010 CFR
2010-10-01
... boundary in which the doors are fitted; (5) Door frames must be of rigid construction and provide at least... inches) square. A self-closing hinged or pivoted steel or equivalent material cover must be fitted in the...) A door in a bulkhead required to be A-60, A-30, or A-15 Class must be of hollow steel or equivalent...
Code of Federal Regulations, 2011 CFR
2011-10-01
... boundary in which the doors are fitted; (5) Door frames must be of rigid construction and provide at least... inches) square. A self-closing hinged or pivoted steel or equivalent material cover must be fitted in the...) A door in a bulkhead required to be A-60, A-30, or A-15 Class must be of hollow steel or equivalent...
49 CFR 393.62 - Emergency exits for buses.
Code of Federal Regulations, 2010 CFR
2010-10-01
... NECESSARY FOR SAFE OPERATION Glazing and Window Construction § 393.62 Emergency exits for buses. (a) Buses... glazing if such glazing is not contained in a push-out window; or, at least 432 cm2 (67 square inches) of free opening resulting from opening of a push-out type window. No area shall be included in this...
46 CFR 151.50-42 - Ethyl ether.
Code of Federal Regulations, 2011 CFR
2011-10-01
... openings shall be in the top of the tank. (2) Pressure vessel type tanks shall be designed for the maximum pressure to which they may be subjected when pressure is used to discharge the cargo, but in no case shall the design pressure be less than 50 pounds per square inch gauge. All openings shall be in the top of...
46 CFR 151.05-1 - Explanation of column headings in Table 151.05.
Code of Federal Regulations, 2013 CFR
2013-10-01
... Ethyl ether”). However, the referenced entry is preferred. (b) Cargo identification/pressure. This column identifies cargo in terms of pressure within the tank. Terms used are: (1) Pressurized. Cargo carried at a pressure in excess of 10 pounds per square inch gauge as measured at the top of the tank (i.e...
46 CFR 151.50-42 - Ethyl ether.
Code of Federal Regulations, 2014 CFR
2014-10-01
... openings shall be in the top of the tank. (2) Pressure vessel type tanks shall be designed for the maximum pressure to which they may be subjected when pressure is used to discharge the cargo, but in no case shall the design pressure be less than 50 pounds per square inch gauge. All openings shall be in the top of...
46 CFR 151.05-1 - Explanation of column headings in Table 151.05.
Code of Federal Regulations, 2011 CFR
2011-10-01
... Ethyl ether”). However, the referenced entry is preferred. (b) Cargo identification/pressure. This column identifies cargo in terms of pressure within the tank. Terms used are: (1) Pressurized. Cargo carried at a pressure in excess of 10 pounds per square inch gauge as measured at the top of the tank (i.e...
46 CFR 151.50-42 - Ethyl ether.
Code of Federal Regulations, 2013 CFR
2013-10-01
... openings shall be in the top of the tank. (2) Pressure vessel type tanks shall be designed for the maximum pressure to which they may be subjected when pressure is used to discharge the cargo, but in no case shall the design pressure be less than 50 pounds per square inch gauge. All openings shall be in the top of...
Fiber sample presentation system for spectrophotometer cotton fiber color measurements
USDA-ARS?s Scientific Manuscript database
The Uster® High Volume Instrument (HVI) is used to class U.S. cotton for fiber color, yielding the industry accepted, cotton-specific color parameters Rd and +b. The HVI examines a 9 square inch fiber sample, and it is also used to test large AMS standard cotton “biscuits” or rectangles. Much inte...
NASA Technical Reports Server (NTRS)
1988-01-01
Instead of bulky coils and compressors used in conventional refrigeration systems, UST design engineers drew on thermo-electric technology. UST's precision temperature chambers (PTC's) feature small thermoelectric modules that measure not much more than 1 square inch and operate on unique phenomenon of heat exchange. When electric current flows through specialized metallic crystals, heat is produced; when current direction is reversed cooling is produced.
Demand Forecasting: An Evaluation of DODs Accuracy Metric and Navys Procedures
2016-06-01
inventory management improvement plan, mean of absolute scaled error, lead time adjusted squared error, forecast accuracy, benchmarking, naïve method...Manager JASA Journal of the American Statistical Association LASE Lead-time Adjusted Squared Error LCI Life Cycle Indicator MA Moving Average MAE...Mean Squared Error xvi NAVSUP Naval Supply Systems Command NDAA National Defense Authorization Act NIIN National Individual Identification Number
Redundant Sensors for Mobile Robot Navigation
1985-09-01
represent a probability that the area is empty, while positive numbers mcan it’s probably occupied. Zero reprtsents the unknown. The basic idea is that...room to give it absolute positioning information. This works by using two infrared emitters and detectors on the robot. Measurements of anglcs are made...meters (T in Kelvin) 273 sec Distances returned when assuming 80 degrees Farenheit , but where. actual temperature is 60 degrees, will be seven inches
An Aerial Radiological Survey of Selected Areas of the City of North Las Vegas
DOE Office of Scientific and Technical Information (OSTI.GOV)
Piotr Wasiolek
2008-06-01
As part of the proficiency training for the Radiological Mapping mission of the Aerial Measuring System (AMS), a survey team from the Remote Sensing Laboratory-Nellis (RSL-Nellis) conducted an aerial radiological survey of selected areas of the city of North Las Vegas for the purpose of mapping natural radiation background and locating any man-made radioactive sources. Survey areas were selected in collaboration with the City Manager's office and included four separate areas: (1) Las Vegas Motor Speedway (10.6 square miles); (2) North Las Vegas Downtown Area (9.2 square miles); (3) I-15 Industrial Corridor (7.4 square miles); and (4) Future site ofmore » University of Nevada Las Vegas campus (17.4 square miles). The survey was conducted in three phases: Phase 1 on December 11-12, 2007 (Areas 1 and 2), Phase 2 on February 28, 2008 (Area 3), and Phase 3 on March 19, 2008 (Area 4). The total completed survey covered a total of 44.6 square miles. The flight lines (without the turns) over the surveyed areas are presented in Figures 1, 2, 3, and 4. A total of eight 2.5-hour-long flights were performed at an altitude of 150 ft above ground level (AGL) with 300 feet of flight-line spacing. Water line and test line flights were conducted over the Lake Mead and Government Wash areas to ensure quality control of the data. The data were collected by the AMS data acquisition system (REDAR V) using an array of twelve 2-inch x 4-inch x 16-inch sodium iodide (NaI) detectors flown on-board a twin-engine Bell 412 helicopter. Data, in the form of gamma energy spectra, were collected continually (every second) over the course of the survey and were geo-referenced using a differential Global Positioning System. Collection of spectral data allows the system to distinguish between ordinary fluctuations in natural background radiation levels and the signature produced by man-made radioisotopes. Spectral data can also be used to identify specific radioactive isotopes. As a courtesy service, with the approval of the U.S. Department of Energy, National Nuclear Security Administration, Nevada Site Office, RSL-Nellis is providing this summary to the office of the Mayor of the City of North Las Vegas along with the gross-count-based exposure rate and man-made count contour maps and GIS shape files in electronic format on a compact disk.« less
Risser, Dennis W.
2008-01-01
This report presents the results of a study by the U.S. Geological Survey, in cooperation with the Pennsylvania Geological Survey, to illustrate a water-budget method for mapping the spatial distribution of ground-water recharge for a 76-square-mile part of the Jordan Creek watershed, northwest of Allentown, in Lehigh County, Pennsylvania. Recharge was estimated by using the Hydrological Evaluation of Landfill Performance (HELP) water-budget model for 577 landscape units in Jordan Creek watershed, delineated on the basis of their soils, land use/land cover, and mean annual precipitation during 1951-2000. The water-budget model routes precipitation falling on each landscape unit to components of evapotranspiration, surface runoff, storage, and vertical percolation (recharge) for a five-layer soil column on a daily basis. The spatial distribution of mean annual recharge during 1951-2000 for each landscape unit was mapped by the use of a geographic information system. Recharge simulated by the water-budget model in Jordan Creek watershed during 1951-2000 averaged 12.3 inches per year and ranged by landscape unit from 0.11 to 17.05 inches per year. Mean annual recharge during 1951-2000 simulated by the water-budget model was most sensitive to changes to input values for precipitation and runoff-curve number. Mean annual recharge values for the crop, forest, pasture, and low-density urban land-use/land-cover classes were similar (11.2 to 12.2 inches per year) but were substantially less for high-density urban (6.8 inches per year), herbaceous wetlands (2.5 inches per year), and forested wetlands (1.3 inches per year). Recharge rates simulated for the crop, forest, pasture, and low-density urban land-cover classes were similar because those land-use/land-cover classes are represented in the model with parameter values that either did not significantly affect simulated recharge or tended to have offsetting effects on recharge. For example, for landscapes with forest land cover, values of runoff-curve number assigned to the model were smaller than for other land-use/land-cover classes (causing more recharge and less runoff), but the maximum depth of evapotranspiration was larger than for other land-use/ land-cover classes because of deeper root penetration in forests (causing more evapotranspiration and less recharge). The smaller simulated recharge for high-density urban and wetland land-use/land-cover classes was caused by the large values of runoff-curve number (greater than 90) assigned to those classes. The large runoff-curve number, however, certainly is not realistic for all wetlands; some wetlands act as areas of ground-water discharge and some as areas of recharge. Simulated mean annual recharge computed by the water-budget model for the 53-square-mile part of the watershed upstream from the streamflow-gaging station near Schnecksville was compared to estimates of recharge and base flow determined by analysis of streamflow records from 1967 to 2000. The mean annual recharge of 12.4 inches per year simulated by the water-budget method for 1967-2000 was less than estimates of mean annual recharge of 19.3 inches per year computed from the RORA computer program and base flow computed by the PART computer program (15.1 inches per year). In theory, the water-budget method provides a practical tool for estimating differences in recharge at local scales of interest, and the watershed- average recharge rate of 12.4 inches per year computed by the method is reasonable. However, the mean annual surface runoff of 4.5 inches per year simulated by the model is unrealistically small. The sum of surface runoff and recharge simulated by the water-budget model (16.9 inches per year) is 7 inches per year less than the streamflow measured at the gaging station near Schnecksville (23.9 inches per year) during 1967-2000, indicating that evapotranspiration is overestimated by the water-budget model by that amount. This discrepancy ca
Effect of fuel volatility on performance of tail-pipe burner
NASA Technical Reports Server (NTRS)
Barson, Zelmar; Sargent, Arthur F , Jr
1951-01-01
Fuels having Reid vapor pressures of 6.3 and 1.0 pounds per square inch were investigated in a tail-pipe burner on an axial-flow-type turbojet engine at a simulated flight Mach number of 0.6 and altitudes from 20,000 to 45,000 feet. With the burner configuration used in this investigation, having a mixing length of only 8 inches between the fuel manifold and the flame holder, the low-vapor-pressure fuel gave lower combustion efficiency at a given tail-pipe fuel-air ratio. Because the exhaust-nozzle area was fixed, the lower efficiency resulted in lower thrust and higher specific fuel consumption. The maximum altitude at which the burner would operate was practically unaffected by the change in fuel volatility.
Improving absolute gravity estimates by the L p -norm approximation of the ballistic trajectory
NASA Astrophysics Data System (ADS)
Nagornyi, V. D.; Svitlov, S.; Araya, A.
2016-04-01
Iteratively re-weighted least squares (IRLS) were used to simulate the L p -norm approximation of the ballistic trajectory in absolute gravimeters. Two iterations of the IRLS delivered sufficient accuracy of the approximation without a significant bias. The simulations were performed on different samplings and perturbations of the trajectory. For the platykurtic distributions of the perturbations, the L p -approximation with 3 < p < 4 was found to yield several times more precise gravity estimates compared to the standard least-squares. The simulation results were confirmed by processing real gravity observations performed at the excessive noise conditions.
Water quality management using statistical analysis and time-series prediction model
NASA Astrophysics Data System (ADS)
Parmar, Kulwinder Singh; Bhardwaj, Rashmi
2014-12-01
This paper deals with water quality management using statistical analysis and time-series prediction model. The monthly variation of water quality standards has been used to compare statistical mean, median, mode, standard deviation, kurtosis, skewness, coefficient of variation at Yamuna River. Model validated using R-squared, root mean square error, mean absolute percentage error, maximum absolute percentage error, mean absolute error, maximum absolute error, normalized Bayesian information criterion, Ljung-Box analysis, predicted value and confidence limits. Using auto regressive integrated moving average model, future water quality parameters values have been estimated. It is observed that predictive model is useful at 95 % confidence limits and curve is platykurtic for potential of hydrogen (pH), free ammonia, total Kjeldahl nitrogen, dissolved oxygen, water temperature (WT); leptokurtic for chemical oxygen demand, biochemical oxygen demand. Also, it is observed that predicted series is close to the original series which provides a perfect fit. All parameters except pH and WT cross the prescribed limits of the World Health Organization /United States Environmental Protection Agency, and thus water is not fit for drinking, agriculture and industrial use.
Predicting the losses in sawtimber volume and quality from fires in oak-hickory forests.
Robert M. Loomis
1974-01-01
Presents a method for predicting future sawtimber losses due to fire-caused wounds. Losses are in terms of: (1) lumber value in dollars, (2) volume in board feet, (3) length of defect in feet, and (4) cross sectional area of defect in square inches. The methods apply to northern red, black, scarlet, white and chestnut oaks.
16 CFR § 1632.4 - Mattress test procedure.
Code of Federal Regulations, 2013 CFR
2013-01-01
... threads per square inch and fabric weight of 3.7±0.8 oz/yd2 (125±28 gm/m2). The size of the sheet or.... The cigarettes shall be positioned directly over the thread or in the depression created by the quilting process on the half of the test surface reserved for bare mattress tests. If the quilt design is...
Procedure for preparation for shipment of natural gas storage vessel
NASA Technical Reports Server (NTRS)
Amawd, A. M.
1974-01-01
A method for preparing a natural gas storage vessel for shipment is presented. The gas is stored at 3,000 pounds per square inch. The safety precautions to be observed are emphasized. The equipment and process for purging the tank and sampling the exit gas flow are described. A diagram of the pressure vessel and the equipment is provided.
1959-12-16
Side view of a F-105B (serial #54-0102) photographed on Rogers Dry Lakebed at Edwards Air Force Base, California in 1959. The black stripes across the left wheel-panel complete the lettering on the bottom of the wing when wheels are retracted. Two of the F-105B characteristics are fuselage length of 61 feet 1.33 inches and a wing area of 385.0 square feet.
Aerial Refueling Boom/Receptacle Guide
2017-07-28
Alleviation System; AR – Aerial Refueling; IDS – Independent Disconnect System; PDL – Pilot Director Lights; PSIG – Pounds per square inch gauge; TMF...proprietary, sensitive, classified or otherwise restricted information. ARSAG documents, as prepared, are not DOD, MOD or NATO standards, but provide...Boom Nozzle Disconnect Provisions, Aerial Refueling Fuel System and Tanker Aids and Cues for the Receiver Aircraft. Also included are Receiver
2015-06-18
x 4 inch square plates. All six plates of each COIC CMC were cut from the same mother panel of the respective material system. Definitive 30...Bibliography [1] W. L. Harper, Isaac Newton’s Scientific Method: Turning Data Into Evidence about Gravity and Cosmology , New York: Oxford University
Handbook for predicting residue weights of Pacific Northwest conifers.
J.A. Kendall Snell; James K. Brown
1980-01-01
Procedures are given forest estimating weights of potential residue from Douglas- fir and western hemlock created by forest management activities west of the summit of the Cascade Range. Preliminary estimates are given for six other species. The weight tables are in pounds per tree and pounds per square foot of basal area for a 6- or 8- inch unmerchantable tip. The...
40 CFR 98.253 - Calculating GHG emissions.
Code of Federal Regulations, 2011 CFR
2011-07-01
... a flare. 0.001 = Unit conversion factor (metric tons per kilogram, mt/kg). n = Number of measurement... average. MVC = Molar volume conversion factor (849.5 scf/kg-mole at 68 °F and 14.7 pounds per square inch... (kg/kg-mole). MVC = Molar volume conversion factor (849.5 scf/kg-mole at 68 °F and 14.7 psia or 836.6...
40 CFR 98.253 - Calculating GHG emissions.
Code of Federal Regulations, 2013 CFR
2013-07-01
... a flare. 0.001 = Unit conversion factor (metric tons per kilogram, mt/kg). n = Number of measurement... average. MVC = Molar volume conversion factor (849.5 scf/kg-mole at 68 °F and 14.7 pounds per square inch... (kg/kg-mole). MVC = Molar volume conversion factor (849.5 scf/kg-mole at 68 °F and 14.7 psia or 836.6...
40 CFR 98.253 - Calculating GHG emissions.
Code of Federal Regulations, 2012 CFR
2012-07-01
... a flare. 0.001 = Unit conversion factor (metric tons per kilogram, mt/kg). n = Number of measurement... average. MVC = Molar volume conversion factor (849.5 scf/kg-mole at 68 °F and 14.7 pounds per square inch... (kg/kg-mole). MVC = Molar volume conversion factor (849.5 scf/kg-mole at 68 °F and 14.7 psia or 836.6...
40 CFR 98.253 - Calculating GHG emissions.
Code of Federal Regulations, 2014 CFR
2014-07-01
... a flare. 0.001 = Unit conversion factor (metric tons per kilogram, mt/kg). n = Number of measurement... average. MVC = Molar volume conversion factor (849.5 scf/kg-mole at 68 °F and 14.7 pounds per square inch... (kg/kg-mole). MVC = Molar volume conversion factor (849.5 scf/kg-mole at 68 °F and 14.7 psia or 836.6...
Characteristics of Five Climax Stands in New Hampshire
W.B. Leak; W.B. Leak
1987-01-01
Analysis of species composition, stand density, and diameter distribution in five climax or old-growth stands in New Hampshire indicates that the northern hardwood climax is characterized by at least 65 to 70 percent tolerant hardwoods, 130 square feet basal area per acre, and "q" ratios (2-inch diameter classes) of 1.3 to 1.4. Climax sprucehemlock have at...
21 CFR 177.1312 - Ethylene-carbon monoxide copolymers.
Code of Federal Regulations, 2014 CFR
2014-04-01
... accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Copies may be obtained from the American Society for...-soluble extractives in each extracting solvent not to exceed 0.5 milligram per square inch of food-contact... copolymer identified in paragraph (a) of this section shall be limited to a thickness of not more than 0.01...
The Wall of Remembrance: Images and Themes of the Holocaust.
ERIC Educational Resources Information Center
Herman, William E.
This pilot study included a content analysis of the Wall of Remembrance (also known as the Childrens Tile Wall) on display at the United States Holocaust Memorial Museum (USHMM) in Washington, D.C. This artwork is composed of 3,324 six-inch square tiles depicting the impressions of children, adolescents and a few adults regarding the Holocaust.…
Experimental investigation of a lightweight rocket chamber
NASA Technical Reports Server (NTRS)
Dalgleish, John E; Tischler, Adelbert O
1953-01-01
Experiments have been conducted with a jacketed rocket combustion chamber that was fabricated by hydraulic-forming from sheet metal. Rocket combustion chambers made by this method have been used successfully. Runs with these combustion chambers have been made at over-all heat-transfer rates 1.7 Btu per square inch per second with water cooling and also ammonia as a regenerative coolant.
NASA Technical Reports Server (NTRS)
Bacon, J. F.
1971-01-01
Emphasis on the consideration of glass formation on a kinetic process made it possible to think of glass compositions different from those normally employed in the manufacture of glass fibers. Approximately 450 new glass compositions were prepared and three dozen of these compositions have values for Young's modulus measured on bulk specimens greater than nineteen million pounds per square inch. Of the new glasses about a hundred could be drawn into fibers by mechanical methods at high speeds. The fiber which has a Young's modulus measured on the fiber of 18.6 million pounds per square inch and has been prepared in quantity as a monofilament (to date more than 150 million lineal feet of 0.2 to 0.4 mil fiber have been produced). This fiber has also been successfully incorporated both in epoxy and polyimide matrices. The epoxy resin composite has shown a modulus forty percent better than that achievable using the most common grade of competitive glass fiber, and twenty percent better than that obtainable with the best available grade of competitive glass fiber. Other glass fibers of even higher modulus have been developed.
Investigation of the fracture mechanics of boride composites
NASA Technical Reports Server (NTRS)
Kaufman, L.; Clougherty, E. V.; Nesor, H.
1971-01-01
Fracture energies of WC-6Co, Boride 5 (ZrB2+SiC), Boride 8(ZrB2+SiC+C) and Boride 8-M2(ZrB2+SiC+C) were measured by slow bend and impact tests of notched charpy bars. Cobalt bonded tungsten carbide exhibited impact energies of 0.76 ft-lb or 73.9 in-lb/square inch. Boride 5 and the Boride 8 exhibit impact energies one third and one quarter of that observed for WC-6Co comparing favorably with measurements for SiC and Si3N4. Slow bend-notched bar-fracture energies for WC-6Co were near 2.6 in-lb/square inch or 1/20 the impact energies. Slow bend energies for Boride 8-M2, Boride 8 and Boride 5 were 58%, 42% and 25% of the value observed for WC-6Co. Fractograph showed differences for WC-6Co where slow bend testing resulted in smooth transgranular cleavage while samples broken by impact exhibited intergranular failures. By contrast the boride fractures showed no distinction based on testing method. Fabrication studies were conducted to effect alteration of the boride composites by alloying and introduction of graphite cloth.
Performance tests of a single-cylinder compression-ignition engine with a displacer piston
NASA Technical Reports Server (NTRS)
Moore, C S; Foster, H H
1935-01-01
Engine performance was investigated using a rectangular displacer on the piston crown to cause a forced air flow in a vertical-disk combustion chamber of a single-cylinder, 4-stroke-cycle compression-ignition engine. The optimum air-flow area was determined first with the area concentrated at one end of the displacer and then with the area equally divided between two passages, one at each end of the displacer. Best performance was obtained with the two-passage air flow arranged to give a calculated maximum air-flow speed of 8 times the linear crank-pin speed. With the same fuel-spray formation as used without the air flow, the maximum clear exhaust brake mean effective pressure at 1,500 r.p.m. was increased from 90 to 115 pounds per square inch and the corresponding fuel consumption reduced from 0.46 to 0.43 pound per brake horsepower-hour. At 1,200 r.p.m., a maximum clear exhaust brake mean effective pressure of 120 pounds per square inch was obtained at a fuel consumption of 0.42 pound per brake horsepower-hour. At higher specific fuel consumption the brake mean effective pressure was still increasing rapidly.
NASA Technical Reports Server (NTRS)
Zettle, Eugene V; Mark, Herman
1953-01-01
The design principle of injecting liquid fuel at more than one axial station in an annual turbojet combustor was investigated. Fuel was injected into the combustor as much as 5 inches downstream of the primary fuel injectors. Many fuel-injection configurations were examined and the performance results are presented for 11 configurations that best demonstrate the trends in performance obtained. The performance investigations were made at a constant combustor-inlet pressure of 15 inches of mercury absolute and at air flows up to 70 percent higher than values typical of current design practice. At these higher air flows, staging the fuel introduction improved the combustion efficiency considerably over that obtained in the combustor when no fuel staging was employed. At air flows currently encountered in turbojet engines, fuel staging was of minor value. Radial temperature distribution seemed relatively unaffected by the location of fuel-injection stations.
Costas loop lock detection in the advanced receiver
NASA Technical Reports Server (NTRS)
Mileant, A.; Hinedi, S.
1989-01-01
The advanced receiver currently being developed uses a Costas digital loop to demodulate the subcarrier. Previous analyses of lock detector algorithms for Costas loops have ignored the effects of the inherent correlation between the samples of the phase-error process. Accounting for this correlation is necessary to achieve the desired lock-detection probability for a given false-alarm rate. Both analysis and simulations are used to quantify the effects of phase correlation on lock detection for the square-law and the absolute-value type detectors. Results are obtained which depict the lock-detection probability as a function of loop signal-to-noise ratio for a given false-alarm rate. The mathematical model and computer simulation show that the square-law detector experiences less degradation due to phase jitter than the absolute-value detector and that the degradation in detector signal-to-noise ratio is more pronounced for square-wave than for sine-wave signals.
Gas-solid fluidized bed reactors: Scale-up, flow regimes identification and hydrodynamics
NASA Astrophysics Data System (ADS)
Zaid, Faraj Muftah
This research studied the scale-up, flow regimes identification and hydrodynamics of fluidized beds using 6-inch and 18- inch diameter columns and different particles. One of the objectives was to advance the scale-up of gas-solid fluidized bed reactors by developing a new mechanistic methodology for hydrodynamic similarity based on matching the radial or diameter profile of gas phase holdup, since gas dynamics dictate the hydrodynamics of these reactors. This has been successfully achieved. However, the literature reported scale-up methodology based on matching selected dimensionless groups was examined and it was found that it was not easy to match the dimensionless groups and hence, there was some deviation in the hydrodynamics of the studied two different fluidized beds. A new technique based on gamma ray densitometry (GRD) was successfully developed and utilized to on-line monitor the implementation of scale-up, to identify the flow regime, and to measure the radial or diameter profiles of gas and solids holdups. CFD has been demonstrated as a valuable tool to enable the implementation of the newly developed scale-up methodology based on finding the conditions that provide similar or closer radial profile or cross sectional distribution of the gas holdup. As gas velocity increases, solids holdup in the center region of the column decreases in the fully developed region of both 6 inch and 18 inch diameter columns. Solids holdup increased with the increase in the particles size and density. Upflowing particles velocity increased with the gas velocity and became steeper at high superficial gas velocity at all axial heights where the center line velocity became higher than that in the wall region. Smaller particles size and lower density gave larger upflowing particles velocity. Minimum fluidization velocity and transition velocity from bubbly to churn turbulent flow regimes were found to be lower in 18 inch diameter column compared to those obtained in 6 inch diameter column. Also the absolute fluctuation of upflowing particles velocity multiplied by solids holdups vś 3ś as one of the terms for solids mass flux estimation was found to be larger in 18-inch diameter column than that in 6-inch diameter column using same particles size and density.
Solar heating system at Security State Bank, Starkville, Mississippi
NASA Technical Reports Server (NTRS)
1980-01-01
The 312 square feet of Solaron flat plate air collectors provide for 788 square feet of space heating, an estimated 55 percent of the heating load. Solar heated air is distributed to the 96 cubic foot steel cylinder, which contains two inch diameter rocks. An air handler unit moves the air over the collector and into the steel cylinder. Four motorized dampers and two gravity dampers are also part of the system. A Solaron controller which has sensors located at the collectors, rock storage, and at the return air, automatically controls the system. Auxiliary heating energy is provided by electric resistance duct heaters.
Small-area snow surveys on the northern plains of North Dakota
Emerson, Douglas G.; Carroll, T.R.; Steppuhn, Harold
1985-01-01
Snow-cover data are needed for many facets of hydrology. The variation in snow cover over small areas is the focus of this study. The feasibility of using aerial surveys to obtain information on the snow water equivalent of the snow cover in order to minimize the necessity of labor intensive ground snow surveys was- evaluated. A low-flying aircraft was used to measure attenuations of natural terrestrial gamma radiation by snow cover. Aerial and ground snow surveys of eight 1-mile snow courses and one 4-mile snow course were used in the evaluation, with ground snow surveys used as the base to evaluate aerial data. Each of the 1-mile snow courses consisted of a single land use and all had the same terrain type (plane). The 4-mile snow course consists of a variety of land uses and the same terrain type (plane). Using the aerial snow-survey technique, the snow water equivalent of the 1-mile snow courses was. measured with three passes of the aircraft. Use of more than one pass did not improve the results. The mean absolute difference between the aerial- and ground-measured snow water equivalents for the 1-mile snow courses was 26 percent (0.77 inches). The aerial snow water equivalents determined for the 1-mile snow courses were used to estimate the variations in the snow water equivalents over the 4-mile snow course. The weighted mean absolute difference for the 4-mile snow course was 27 percent (0.8 inches). Variations in snow water equivalents could not be verified adequately by segmenting the aerial snow-survey data because of the uniformity found in the snow cover. On the 4-mile snow coirse, about two-thirds of the aerial snow-survey data agreed with the ground snow-survey data within the accuracy of the aerial technique ( + 0.5 inch of the mean snow water equivalent).
A Moiré Pattern-Based Thread Counter
NASA Astrophysics Data System (ADS)
Reich, Gary
2017-10-01
Thread count is a term used in the textile industry as a measure of how closely woven a fabric is. It is usually defined as the sum of the number of warp threads per inch (or cm) and the number of weft threads per inch. (It is sometimes confusingly described as the number of threads per square inch.) In recent years it has also become a subject of considerable interest and some controversy among consumers. Many consumers consider thread count to be a key measure of the quality or fineness of a fabric, especially bed sheets, and they seek out fabrics that advertise high counts. Manufacturers in turn have responded to this interest by offering fabrics with ever higher claimed thread counts (sold at ever higher prices), sometime achieving the higher counts by distorting the definition of the term with some "creative math." In 2005 the Federal Trade Commission noted the growing use of thread count in advertising at the retail level and warned of the potential for consumers to be misled by distortions of the definition.
Space Launch Initiative (SLI) Engine Test
NASA Technical Reports Server (NTRS)
2002-01-01
NASA's Marshall Space Flight Center (MSFC) in Huntsville, Alabama, has begun a series of engine tests on the Reaction Control Engine developed by TRW Space and Electronics for NASA's Space Launch Initiative (SLI). SLI is a technology development effort aimed at improving the safety, reliability, and cost effectiveness of space travel for reusable launch vehicles. The engine in this photo, the first engine tested at MSFC that includes SLI technology, was tested for two seconds at a chamber pressure of 185 pounds per square inch absolute (psia). Propellants used were liquid oxygen as an oxidizer and liquid hydrogen as fuel. Designed to maneuver vehicles in orbit, the engine is used as an auxiliary propulsion system for docking, reentry, fine-pointing, and orbit transfer while the vehicle is in orbit. The Reaction Control Engine has two unique features. It uses nontoxic chemicals as propellants, which creates a safer environment with less maintenance and quicker turnaround time between missions, and it operates in dual thrust modes, combining two engine functions into one engine. The engine operates at both 25 and 1,000 pounds of force, reducing overall propulsion weight and allowing vehicles to easily maneuver in space. The force of low level thrust allows the vehicle to fine-point maneuver and dock, while the force of the high level thrust is used for reentry, orbital transfer, and course positioning.
1987-12-01
pressure between two Mach 3 flows approachs absolute zero , Pb=.04 psia for Pop= 100 psia. However, viscous effects increase the base pressure. Korst theory...this problem. Acetylene was chosen as the primary fuel because of its relatively low spontaneous ignition temperature, 581 degrees Farenheit , and high...with the corresponding test section. The exit dimension could be adjusted with a screw mechanism from zero to 2.625 inches. A bracket to hold a .250
Reinforced Concrete Wall Form Design Program
1992-08-01
criteria is an absolute limit. You have the choice of 1/8 or 1/16 of an inch total deflection in a span. Once these limits are set here, then they are...Calls GET-INFO-TEXT - Calls ZERO -PLY - If the response to GET-INFO-TEXT is "Values retrieved by computer", then the following procedures are executed...like to enter their own values. ZERO -PLY - Re-initializes all PLY-VEC values to"?". GET-PLY-CLASS - Retrieves from the user the grade of plyform to be
Porter, Nicholas J.; Bonvechio, Timothy F.; McCormick, Joshua L.; Quist, Michael
2014-01-01
The objectives of this study were to evaluate the population dynamics of bowfin (Amia calva) in Lake Lindsay Grace, Georgia, and to compare those dynamics to other bowfin populations. Relative abundance of bowfin sampled in 2010 in Lake Lindsay Grace was low and variable (mean±SD; 2.7±4.7 fish per hour of electrofishing). Total length (TL) of bowfin collected in Lake Lindsay Grace varied from 233–683 mm. Age of bowfin in Lake Lindsay Grace varied from 0–5 yr. Total annual mortality (A) was estimated at 68%. Both sexes appeared to be fully mature by age 2 with gonadosomatic index values above 8 for females and close to 1 for males. The majority of females were older, longer, and heavier than males. Bowfin in Lake Lindsay Grace had fast growth up to age 4 and higher total annual mortality than the other populations examined in this study. A chi-square test indicated that size structure of bowfin from Lake Lindsay Grace was different than those of a Louisiana population and two bowfin populations from the upper Mississippi River. To further assess bowfin size structure, we proposed standard length (i.e., TL) categories: stock (200 mm, 8 inches), quality (350 mm, 14 inches), preferred (460 mm, 18 inches), memorable (560 mm, 22, inches), and trophy (710 mm, 28 inches). Because our knowledge of bowfin ecology is limited, additional understanding of bowfin population dynamics provides important insight that can be used in management of bowfin across their distribution.
The EPA is taking final action to relax the federal volatility (RVP) standard applicable to summer gasoline supplied to three areas in Florida and the Triangle and Triad Areas in North Carolina from 7.8 pounds per square inch (psi) to 9.0 psi.
Economies of scale and trends in the size of southern forest industries
James E. Granskog
1978-01-01
In each of the major southern forest industries, the trend has been toward achieving economies of scale, that is, to build larger production units to reduce unit costs. Current minimum efficient plant size estimated by survivor analysis is 1,000 tons per day capacity for sulfate pulping, 100 million square feet (3/8- inch basis) annual capacity for softwood plywood,...
Tree injuries from mechanized logging
Richard M. Godman
1992-01-01
Small trees in even-aged northern hardwood stands suffer the most mechanical damage when stands are thinned for the first time. From 15 to 35 percent of the trees may be damaged; a quarter of the trees (but usually less than 20 per acre) can be seriously damaged by having at least 50 square inches of the cambium exposed. Bole damage is most common, followed by root and...
Kolodney, M.
1959-02-01
A method is presented for effecting eloctrolytic dissolution of a metallic uranium article at a uniform rate. The uranium is made the anode in an aqueous phosphoric acid solution containing nitrate ions furnished by either ammonium nitrate, lithium nitrate, sodium nitrate, or potassium nitrate. A stainless steel cathode is employed and electrolysls carried out at a current density of about 0.1 to 1 ampere per square inch.
2013-12-05
pressure (see Section 2.3) - Optional 1 percent Tire pressure 0.7 kilopascals (kPa) (0.1 pounds per square inch (psi)) Brake pedal application...d. Load cell to monitor brake pedal force with a range of 0 to 136 kg (0 to 300 lb) and accuracy + 1.0 percent full scale. While brake pedal ...sideslip, brake pedal application force and document the manufacturer, identification (serial number, part number, etc.), calibration information
Growth of planted ponderosa pine thinned to different stocking levels in northern California
William W. Oliver
1979-01-01
Growth was strongly related to growing stock level (GSL) for 5 years after thinning 20-year-old poles on Site Index50 115 land at the Elliot Ranch Plantation in northern California. Five GSL's-basal areas anticipated when trees average 10 inches d.b.h. or more-ranging from 40 to 160 square feet per acre were tested. Periodic annual increment...
The Pine-Popple River basin--Hydrology of a wild river area, northeastern Wisconsin
Oakes, Edward L.; Field, Stephen J.; Seeger, Lawrence P.
1973-01-01
The Pine and Popple Rivers, virtually unaltered by man, flow through a semiprimitive area of forests, lakes, and glacial hills. White-water streams, natural lakes, fish and animal life, and abundant vegetation contribute to the unique recreational and aesthetic characteristics of the area. Resource planning or development should recognize the interrelationships within the hydrologic system and the possible effects of water and land-use changes upon the wild nature of the area. The basin covers about 563 square miles in northeastern Wisconsin. Swamps and wetlands cover nearly 110 square miles, and the 70 lakes cover about 11 square miles. The undulating topography is formed by glacial deposits overlying an irregular, resistant surface of bedrock. An annual average of 30 inches of precipitation, highest from late spring to early autumn, falls on the basin. Of this amount, evapotranspiration, highest in mid summer and late summer, averages 19 inches; the remaining 11 inches is runoff, which is highest in spring and early summer. Ground water from the glacial drift is the source of water for the minor withdrawal use in the basin. Ground-water movement is to streams and lakes and regionally follows the slope of topography and the bedrock surface, which is generally west to east. Ground water is of good quality, although locally high in iron. The major uses of water are for recreation and power generation. Domestic use is slight. No water is withdrawn from lakes or streams, and no sewage or industrial wastes are added to lakes or streams. Most of the flow of the Pine River is used for power generation. The main stems of the Pine and Popple Rivers contain 114 canoeable miles, of which 95 percent is without such major obstructions as falls or large rapids. In general streams support cold-water fish, and lakes support warm-water fish. Trout is the principal stream and game fish in the basin. The basin has no significant water problems. Future development between the Pine River power plant and the mouth of the Pine River should have little effect on the western two-thirds of the basin, already largely protected by public ownership or development planning agreements.
Major winter and nonwinter floods in selected basins in New York and Pennsylvania
Langbein, Walter Basil
1947-01-01
The scientific design of flood-control works is based on an evaluation of the hydrologic factors basic to flood events, particularly how rainfall and snow runoff, soil conditions, and channel influences can combine to produce greater or lesser floods. For this purpose an analysis of the pertinent hydrologic data is needed. The methods of analysis adopted should conform as closely as possible to those already in use and must be adapted to the quality of the available information. Maximum floods in 8 basins in New York and Pennsylvania during the winter and nonwinter months were studied, a total of 21 floods. The most outstanding winter flood of record in the North Atlantic region was that of March 1936. Rainfall plus snow melt in the basins studied ranged between 3.04 and 6.87 inches, and associated volumes of direct runoff from 1.88 to 5.63 inches. Winter floods have a common characteristic in their relation to freezing temperature. The antecedent periods, representing a period of snow accumulation and frost penetration, are below freezing, and the flood itself is contemporaneous with a period of above-freezing temperatures, usually associated with rain, during which the previously accumulated snow is melted. A second common characteristic of major winter floods is their tendency to be associated with widespread causal meteorologic conditions. There was a more complete conversion of rainfall and snow melt into runoff during the winter storms studied than during the wettest nonwinter flood. Snow melt during winter floods ranged from 0.04 to 0.07 inch per degree-day above 32° F. The depth of mean areal rainfall produced by the nonwinter storms studied ranged from 3.05 to 4.96 inches. The maximum 24-hour quantity at single stations was 14 inches, which was measured during the storm of July 1935 in New York. The volume of direct runoff ranged between 1.39 and 3.41 inches. The portion of rainfall that was converted into runoff varied in accordance with the rate of antecedent base flow, expressed in second-feet per square mile, and emphasized the influence of antecedent conditions. The average volume of direct runoff during winter floods was 4.24 inches, and the average during nonwinter floods was 2.44 inches. The latter, however, were more concentrated as to time, tending to compensate for large volume of runoff in winter, so that the crest rates of direct runoff averaged 0.056 inches per hour during the winter and 0.051 inches during the nonwinter period.
Jarrott, L. C.; Wei, M. S.; McGuffey, C.; ...
2017-04-27
Here, we have built an absolutely calibrated, highly efficient, Bragg crystal spectrometer in von Hamos geometry. This zinc von Hamos spectrometer uses a crystal made from highly oriented pyrolytic graphite that is cylindrically bent along the non-dispersive axis. It is tuned to measure x-ray spectra in the 7–10 keV range and has been designed to be used on a Ten Inch Manipulator for the Omega and OmegaEP target chambers at the Laboratory for Laser Energetics in Rochester, USA. Significant shielding strategies and fluorescence mitigation have been implemented in addition to an imaging plate detector making it well suited for experimentsmore » in high-intensity environments. Here we present the design and absolute calibration as well as mosaicity and integrated reflectivity measurements.« less
Growth after thinning ponderosa and Jeffrey pine pole stands in northeastern California
William W. Oliver
1972-01-01
Thinning ponderosa and Jeffrey pine pole stands (6 to 8 inches d.b.h.) on Meyer Site Classes IV and V land (site index 65 to 80) stimulates growth in diameter and height. This was concluded from data on 12 thinned plots scattered over northeastern California, in natural stands and in a plantation. Basal areas immediately after thinning ranged from 13 to 149 square feet...
James M. Guldin; Thomas Foti
2004-01-01
Abstract - Baseline tree data were collected in four watersheds in the eastern Ouachita Mountains during 1996-98. By watershed, average basal area ranged from 71 to 102 square feet per acre, average tree density ranged from 234 to 295 trees per acre, and quadratic mean diameter of trees ranged from 7.41 to 8.22 inches. Variables for which the largest...
Closeup View of Compacted Soil
NASA Technical Reports Server (NTRS)
2004-01-01
Soil on Mars can be a bit clumpy, as shown in this image of soil after it was compacted by one of the wheels of NASA's Mars Exploration Rover Spirit. Scientists think the light-colored material may be a global layer of airfall dust. Spirit's microscopic imager took this picture, showing an area approximately 3 centimeters (1.2 inches) square, during the rover's 314th martian day, or sol (Nov. 19, 2004).NASA Technical Reports Server (NTRS)
Baghdadi, A.; Gurtler, R. W.; Legge, R.; Sopori, B.; Rice, M. J.; Ellis, R. J.
1979-01-01
A technique for growing limited-length ribbons continually was demonstrated. This Rigid Edge technique can be used to recrystallize about 95% of the polyribbon feedstock. A major advantage of this method is that only a single, constant length silicon ribbon is handled throughout the entire process sequence; this may be accomplished using cassettes similar to those presently in use for processing Czochralski waters. Thus a transition from Cz to ribbon technology can be smoothly affected. The maximum size being considered, 3 inches x 24 inches, is half a square foot, and will generate 6 watts for 12% efficiency at 1 sun. Silicon dioxide has been demonstrated as an effective, practical diffusion barrier for use during the polyribbon formation.
Feasibility of an advanced thrust termination assembly for a solid propellant rocket motor
NASA Technical Reports Server (NTRS)
1975-01-01
A total of 68 quench tests were conducted in a vented bomb assembly (VBA). Designed to simulate full-scale motor operating conditions, this laboratory apparatus uses a 2-inch-diameter, end-burning propellant charge and an insulated disc of consolidated hydrated aluminum sulfate along with the explosive charge necessary to disperse the salt and inject it onto the burning surface. The VBA was constructed to permit variation of motor design parameters of interest; i.e., weight of salt per unit burning surface area, weight of explosive per unit weight of salt, distance from salt surface to burning surface, incidence angle of salt injection, chamber pressure, and burn time. Completely satisfactory salt quenching, without re-ignition, occurred in only two VBA tests. These were accomplished with a quench charge ratio (QCR) of 0.023 lb salt per square inch of burning surface at dispersing charge ratios (DCR) of 13 and 28 lb of salt per lb of explosive. Candidate materials for insulating salt charges from the rocket combustion environment were evaluated in firings of 5-inch-diameter, uncured end-burner motors. A pressed, alumina ceramic fiber material was selected for further evaluation and use in the final demonstration motor.
Durbin, Timothy J.
1974-01-01
The Stanford Watershed Model was used to simulate the effects of urbanization on the discharge from five drainage basins in the upper Santa Ana Valley, an area with an average annual precipitation of 15 inches. The drainage basins ranged in size from 3.72 to 83.4 square miles. Using the model, synthetic records of streamflow for each basin were generated to represent various degrees of urban development. Examination of the synthetic records indicated that urbanization has the following effects on streamflow in the area:Average annual runoff from a drainage basin with an effective impervious area of 10 percent of the drainage area is approximately 2 inches, and increases by 1 inch for each increase in effective impervious cover equal to 10 percent of the drainage area. About 30 percent of a fully urbanized area is effectively impervious.Urbanization can increase the magnitude of peak discharge and daily mean discharge with a recurrence interval of 2 years by a factor of three to six.Peak discharges and daily mean discharges that have recurrence intervals greater than a limiting value ranging from 50 to 200 years or more are little affected by urbanization.
NASA Technical Reports Server (NTRS)
2008-01-01
This is a photo of an engineering model of the Thermal and Evolved-Gas Analyzer (TEGA) instrument on board NASA's Phoenix Mars Lander. This view shows a TEGA oven-loading mechanism beneath the input screen. The screen on the 1-and-1/2-inch-wide funnel has been removed in this model to show the whirligig that is suspended from the screw on the shaft. The black hole underneath is the porthole that leads to the oven. A tiny electric current compresses and releases a spring on the shaft. As the shaft spins, the screw bumps the screen, breaking up clumps of material into fine particles so they pass through the one millimeter-square screen openings. The energy applied to the tapping screen is about 0.02 inch per pound, or the force needed to move a one-pound mass two-hundredths of an inch. The screw also lifts the three-bladed whirligig so that it jostles fine particles and keeps the oven port open to aid the loading process. The Phoenix Mission is led by the University of Arizona, Tucson, on behalf of NASA. Project management of the mission is by NASA's Jet Propulsion Laboratory, Pasadena, Calif. Spacecraft development is by Lockheed Martin Space Systems, Denver.Development of Ceramic Fibers for Reinforcement in Composite Materials
NASA Technical Reports Server (NTRS)
Gates, L. E.; Lent, W. E.; Teague, W. T.
1961-01-01
Refinements of the vertical arc fiberizing apparatus resulted in its ability to fiberize very different refractory glasses having wide ranges of properties. Although the apparatus, was originally designed as a laboratory research tool for the evaluation of many compositions daily, up to one quarter pound of fibers of a single composition could be produced in an 8-hour day. Fibers up to six and a half feet long were produced with the apparatus. Studies were conducted of two methods of fiberizing refractory glasses requiring rapid freezing from the melt. The first method consisted of fiberizing droplets of molten glass passing through an annular nozzle. The second method consisted of reconstructing the annular nozzle in. the shape of a horseshoe to achieve a shorter delay in blasting a molten droplet from the tip of a rod. Both methods were judged feasible for producing fibers of glasses requiring rapid freezing. The first method would be more amenable to volume fiber production. Studies of induction heating for fiber formation did not lead to its designation as a very efficient heating method. Problems. remain to be solved, in the design of a suitable susceptor for a higher heating rate, in protecting the susceptor from oxidation with an inert gas, in contamination of the melt from a refractory crucible, and in the protective radiation shielding of the induction concentrator coil. It is not considered practical to continue studies of this heating method. In the course of this program 151 refractory glass compositions were evaluated for fiber, forming characteristics. Of the various types of materials studied, the following showed promise in producing acceptable refractory fibers: sIlica- spinel (magnesium aluminate), silica- spinel-zirconia, silica-zirconia, silica-zinc spinel, aluminum phosphate glasses, and fluoride glasses. Compositions which did not produce acceptable fibers were high zirconia materials, barium spinels, and calcium aluminates. Improvements in the. testing apparatus for single fiber tensile strength increased the precision. of tests conducted on nine fibers. The highest mean tensile strength, a value of 295,000 pounds per square inch, was obtained with R-141 fibers. Treatment of R-74 fibers with anhydrous Linde A-1100 silane finish improved its mean fiber tensile strength by 25 percent. The lapse of time after fiber formation had no measurable effect on tensile strength. A static heating test conducted with various high melting fibers indicated that Fiberfrax and R-108 underwent no significant changes in bulk volume or resiliency on exposure to 2750 degrees Fahrenheit (1510 degrees Centigrade) in an oxidizing atmosphere. For fiber-resin composition fabrication, ten fiber materials were selected on the bases of high fiber yield, fusion temperature, and type of composition. Fiberfrax, a commercial ceramic fiber, was included for comparison. A new, more effective method of removing pellets from blown fibers was developed. The de-pelletized fibers were treated with a silane finish and felted into ten-inch diameter felts prior to resin impregnation. Composites containing 30 percent by weight of CTL 91-LD phenolic resin were molded under high pressure from the impregnated felts and post-cured to achieve optimum properties. Flexural strength, flexural modules of elasticity, and punch shear strength tests were conducted on the composite specimens. The highest average flexural strength obtained was 19,958 pounds per square inch with the R-74-fiber-resin composite. This compares very favorably with the military specification of 13,000 pounds per square inch flexural strength for randomly oriented fiber reinforced composites. The highest punch shear strength (11,509 pounds per square inch) was obtained with the R-89 fiber-resin composite. The effects of anhydrous fiber finishes on composite strength were not clearly indicated. Plasma arc tests at a heat flux of 550 British Thermal Units per square foot per second on eight composite materials indicated ablation rates generally equivalent to Fiberglas-Micarta No. 259-2. The composite reinforced with R-99 fibers had an average ablation rate of 0.008 inch per second and appears quite promising on the basis of these tests. Preliminary studies for processing fibers into yarn and fabric were conducted with R-99 fibers. The use of certain organic gums aided in 2 fabricating by hand several relatively strong yarns and a crude fabric swatch. This indicated the practicality of developing techniques for processing these fibers into yarn and fabric without significant damage to the fibers.
Estimation of selected seasonal streamflow statistics representative of 1930-2002 in West Virginia
Wiley, Jeffrey B.; Atkins, John T.
2010-01-01
Regional equations and procedures were developed for estimating seasonal 1-day 10-year, 7-day 10-year, and 30-day 5-year hydrologically based low-flow frequency values for unregulated streams in West Virginia. Regional equations and procedures also were developed for estimating the seasonal U.S. Environmental Protection Agency harmonic-mean flows and the 50-percent flow-duration values. The seasons were defined as winter (January 1-March 31), spring (April 1-June 30), summer (July 1-September 30), and fall (October 1-December 31). Regional equations were developed using ordinary least squares regression using statistics from 117 U.S. Geological Survey continuous streamgage stations as dependent variables and basin characteristics as independent variables. Equations for three regions in West Virginia-North, South-Central, and Eastern Panhandle Regions-were determined. Drainage area, average annual precipitation, and longitude of the basin centroid are significant independent variables in one or more of the equations. The average standard error of estimates for the equations ranged from 12.6 to 299 percent. Procedures developed to estimate the selected seasonal streamflow statistics in this study are applicable only to rural, unregulated streams within the boundaries of West Virginia that have independent variables within the limits of the stations used to develop the regional equations: drainage area from 16.3 to 1,516 square miles in the North Region, from 2.78 to 1,619 square miles in the South-Central Region, and from 8.83 to 3,041 square miles in the Eastern Panhandle Region; average annual precipitation from 42.3 to 61.4 inches in the South-Central Region and from 39.8 to 52.9 inches in the Eastern Panhandle Region; and longitude of the basin centroid from 79.618 to 82.023 decimal degrees in the North Region. All estimates of seasonal streamflow statistics are representative of the period from the 1930 to the 2002 climatic year.
NASA Astrophysics Data System (ADS)
Chenciner, Alain; Venturelli, Andrea
2000-09-01
We consider the problem of 4 bodies of equal masses in R 3 for the Newtonian r-1 potential. We address the question of the absolute minima of the action integral among (anti)symmetric loops of class H 1 whose period is fixed. It is the simplest case for which the results of [4] (corrected in [5]) do not apply: the minima cannot be the relative equilibria whose configuration is an absolute minimum of the potential among the configurations having a given moment of inertia with respect to their center of mass. This is because the regular tetrahedron cannot have a relative equilibrium motion in R 3 (see [2]). We show that the absolute minima of the action are not homographic motions. We also show that if we force the configuration to admit a certain type of symmetry of order 4, the absolute minimum is a collisionless orbit whose configuration ‘hesitates’ between the central configuration of the square and the one of the tetrahedron. We call these orbits ‘hip-hop’. A similar result holds in case of a symmetry of order 3 where the central configuration of the equilateral triangle with a body at the center of mass replaces the square.
NASA Technical Reports Server (NTRS)
Bless, R. C.; Code, A. D.; Fairchild, E. T.
1976-01-01
The absolute energy distribution in the ultraviolet is given for the stars alpha Vir, eta UMa, and alpha Leo. The calibration is based on absolute heterochromatic photometry between 2920 and 1370 A carried out with an Aerobee sounding rocket. The fundamental radiation standard is the synchrotron radiation from 240-MeV electrons in a certain synchrotron storage ring. On the basis of the sounding-rocket calibration, the preliminary OAO-2 spectrometer calibration has been revised; the fluxes for the three program stars are tabulated in energy per second per square centimeter per unit wavelength interval.
1982-01-01
second) Dia propeller diameter (expressed in inches) T°F air temperature in degrees Farenheit T°C air temperature in degrees Celsius T:dBA total dBA...eMpiriC31 function to the absolute noise level ordinate. The term 240 log ( MH is the most sensitive and important part of the equation. The constant (240...standard day, zero wind, dry, zero gradient runway, at a sea level airport. 2. All aircraft operate at maximum takeoff gross weight. 3. All aircraft climb
Cooling Characteristics of a 2-Row Radial Engine
NASA Technical Reports Server (NTRS)
Schey, Oscar W; Rollin, Vern G
1937-01-01
This report presents the results of cooling tests conducted on a calibrated GR-1535 Pratt and Whitney Wasp, Jr. Engine installed in a Vought X04U-2 airplane. The tests were made in the NACA full-scale tunnel at air speeds from 70 to 120 miles per hour, at engine speeds from 1,500 to 2,600 r.p.m., and at manifold pressures from 19 to 33 inches of mercury absolute. A Smith controllable propeller was used to facilitate obtaining the different combinations of engine speed, power, and manifold pressure.
NASA Technical Reports Server (NTRS)
Finger, Harold B.; Schum, Harold J.; Buckner, Howard Jr.
1947-01-01
Effect of inlet-air pressure and temperature on the performance of the X24-2 10-Stage Axial-Flow Compressor from the X24C-2 turbojet engine was evaluated. Speeds of 80, 89, and 100 percent of equivalent design speed with inlet-air pressures of 6 and 12 inches of mercury absolute and inlet-air temperaures of approximately 538 degrees, 459 degrees,and 419 degrees R ( 79 degrees, 0 degrees, and minus 40 degrees F). Results were compared with prior investigations.
Work Plan and Field Sampling Plan Site Investigations Fort Devens, Massachusetts
1992-02-01
Plan PPE Personal Protective Equipment PPM Parts Per Million PRI Potomac Research , Inc. PSI Pounds Per Square Inch PVC Polyvinyl Chloride QAPjP Quality...Aquifers with Completely or Partially Penetrating Wells, Water Resources Research , 12: 423-428. Brackley, Richard A. and B. P. Hansen, 1977, Water...of a Finite Diameter Well to an Instantaneous Charge of Water, Water Resources Research , 3: 263-269. Directorate of Engineering and Housing (DEH
Ponderosa pine mortality resulting from a mountain pine beetle outbreak
William F. McCambridge; Frank G. Hawksworth; Carleton B. Edminster; John G. Laut
1982-01-01
From 1965 to 1978, mountain pine beetles killed 25% of the pines taller than 4.5 feet in a study area in north-central Colorado. Average basal area was reduced from 92 to 58 square feet per acre. Mortality increased with tree diameter up to about 9 inches d.b.h. Larger trees appeared to be killed at random. Mortality was directly related to number of trees per acre and...
Installation package for air flat plate collector
NASA Technical Reports Server (NTRS)
1977-01-01
The Solar 2 dimensions are four feet by eight feet by two and one half inches. The collector weighs 130 pounds and has an effective solar collection area of over 29.5 square feet. This area represents 95 percent of the total surface of the collector. The installation, operation and maintenance manual, safety hazard analysis, special handling instructions, materials list, installation concept drawings, warranty and certification statement are included in the installation package.
NASA Technical Reports Server (NTRS)
Nieh, C. Y.; Wallace, J. F.
1981-01-01
Sputtered coatings of Mo, W, Pt, Ag, Au, Co, Cr, Ni, Ag + Cu, Mo + Pt, Si3N4, A1N, Cr3C2, Ta5Si3, and ZrO2 were applied to a 2-inch-square, 7-inch-long thermal fatigue test specimen which was then internally water cooled and alternately immersed in molten aluminum and cooled in air. After 15,000 cycles the thermal fatigue cracks at the specimen corners were measured. Results indicate that a significant improvement in thermal fatigue resistance was obtained with platinum, molybdenum, and tungsten coatings. Metallographic examination indicates that the improvement in thermal fatigue resistance resulted from protection of the surface of the die steel from oxidation. The high yield strength and ductility of molybdenum and tungsten contributed to the better thermal fatigue resistance.
Inhibition of Titanium In Fuming Nitric Acid
DOE Office of Scientific and Technical Information (OSTI.GOV)
RITTENHOUSE, J. B.; PAPP, C. A.
1958-06-01
Storage tests were conducted to determine the effectiveness of oxygen in inhibiting the corrosion reaction of titanium in fuming nitric acid (FNA). In these tests, which were of 28 days duration at a temperature of 30 C, the samples investigated were ½-inch squares (0.020 inch thick) of commercially pure titanium (75A) and a binary 8 percent-manganese alloy (C110M). The specimens were stored in Teflon-lined aluminum pressure vessels at 50 percent ullage. The pressure vessels were of the following types: vented to the atmosphere, sealed with air in the vapor space, sealed with oxygen atmosphere in the vapor space, and equippedmore » for a 1-ml/minute oxygen flow through the vapor space. Finally, results of the investigation indicated no inhibition of titanium corrosion by oxygen, but confirmed the inhibiting effect of a water content of 1 to 2 percent by weight in the FNA.« less
Practical low-cost stereo head-mounted display
NASA Astrophysics Data System (ADS)
Pausch, Randy; Dwivedi, Pramod; Long, Allan C., Jr.
1991-08-01
A high-resolution head-mounted display has been developed from substantially cheaper components than previous systems. Monochrome displays provide 720 by 280 monochrome pixels to each eye in a one-inch-square region positioned approximately one inch from each eye. The display hardware is the Private Eye, manufactured by Reflection Technologies, Inc. The tracking system uses the Polhemus Isotrak, providing (x,y,z, azimuth, elevation and roll) information on the user''s head position and orientation 60 times per second. In combination with a modified Nintendo Power Glove, this system provides a full-functionality virtual reality/simulation system. Using two host 80386 computers, real-time wire frame images can be produced. Other virtual reality systems require roughly 250,000 in hardware, while this one requires only 5,000. Stereo is particularly useful for this system because shading or occlusion cannot be used as depth cues.
NASA Technical Reports Server (NTRS)
Nemeth, Z. N.
1974-01-01
Two coatings for a Rayleigh step thrust bearing were tested when coasting down and stopping under self-acting operation in air. The thrust bearing had an outside diameter of 8.9 cm (3.5 in.), an inside diameter of 5.4 cm (2.1 in.), and nine sectors. The load was 73 N (16.4 lbf). The load pressure was 19.1 kN/per square meter (2.77 lbf/per square inch) on the total thrust bearing area. The chromium oxide coating was good to 150 stops without bearing deterioration, and the molybdenum disulfide coating was good for only four stops before bearing deterioration. The molybdenum disulfide coated bearing failed after nine stops.
Manufacturing Process Development to Produce Depleted Uranium Wire for EBAM Feedstock
DOE Office of Scientific and Technical Information (OSTI.GOV)
Alexander, David John; Clarke, Kester Diederik; Coughlin, Daniel Robert
2015-06-30
Wire produced from depleted uranium (DU) is needed as feedstock for the Electron-Beam Additive Manufacturing (EBAM) process. The goal is to produce long lengths of DU wire with round or rectangular cross section, nominally 1.5 mm (0.060 inches). It was found that rolling methods, rather than swaging or drawing, are preferable for production of intermediate quantities of DU wire. Trials with grooveless rolling have shown that it is suitable for initial reductions of large stock. Initial trials with grooved rolling have been successful, for certain materials. Modified square grooves (square round-bottom vee grooves) with 12.5 % reduction of area permore » pass have been selected for the reduction process.« less