Add to ORKGPerformance evaluation tests on flexible pressure hose in Saturn ground support equipmen
Experimental design and performance data on carbon dioxide and oxygen control for portable life supp...
During the summer of 1990, space shuttle Columbia experienced both an external tank/orbiter disconne...
Thruster valve assemblies (T/VA's) were subjected to the development test program for the combined J...
Leakage testing handbook giving fundamentals, theory, methods, detector equipment, and test medi
Machined polyimide second-stage rod seals were evaluated to determine their suitability for single-s...
Surveyor Vernier thrust chamber assembly - bipropellant rocket engine, flow control, control interfa...
Environment and function testing of pressure transducer used for hydraulic accumulator pressure indi...
Space Shuttle Flight Support Motor No. 1 (FSM-1) was static test fired on 15 Aug. 1990 at the Thioko...
Functional and environment testing of 8-inch valve used in vaporizer units and umbilical tower hydro...
A test was conducted to evaluate the fire containment characteristics of a Boeing 747 lavatory modul...
Heat transfer data for the 0.0175-scale space shuttle vehicle 3 are presented. Interference heating ...
Continuing efforts in large gains in heat-pipe performance are reported. It was found that gas-contr...
A detailed description of a computer model that has been developed for assessing the feasibility of ...
Qualification testing of pressure gauge used at Cape Kennedy in launch complex 34 pneumatic distribu...
The aerodynamic effects of plumes from hot combustion gases in the presence of a transonic external ...
Experimental design and performance data on carbon dioxide and oxygen control for portable life supp...
During the summer of 1990, space shuttle Columbia experienced both an external tank/orbiter disconne...
Thruster valve assemblies (T/VA's) were subjected to the development test program for the combined J...
Leakage testing handbook giving fundamentals, theory, methods, detector equipment, and test medi
Machined polyimide second-stage rod seals were evaluated to determine their suitability for single-s...
Surveyor Vernier thrust chamber assembly - bipropellant rocket engine, flow control, control interfa...
Environment and function testing of pressure transducer used for hydraulic accumulator pressure indi...
Space Shuttle Flight Support Motor No. 1 (FSM-1) was static test fired on 15 Aug. 1990 at the Thioko...
Functional and environment testing of 8-inch valve used in vaporizer units and umbilical tower hydro...
A test was conducted to evaluate the fire containment characteristics of a Boeing 747 lavatory modul...
Heat transfer data for the 0.0175-scale space shuttle vehicle 3 are presented. Interference heating ...
Continuing efforts in large gains in heat-pipe performance are reported. It was found that gas-contr...
A detailed description of a computer model that has been developed for assessing the feasibility of ...
Qualification testing of pressure gauge used at Cape Kennedy in launch complex 34 pneumatic distribu...
The aerodynamic effects of plumes from hot combustion gases in the presence of a transonic external ...
Experimental design and performance data on carbon dioxide and oxygen control for portable life supp...
During the summer of 1990, space shuttle Columbia experienced both an external tank/orbiter disconne...
Thruster valve assemblies (T/VA's) were subjected to the development test program for the combined J...