Reactivity and expansion characteristics of Aerozine-50 and nitrogen tetroxide from vacuum chamber test
Strain gages, nitrocellulose effects, and mathematical models for hypervelocity launch tubes with pr...
Structure and flow properties of liquid nitrogen and liquid oxygen difluoride gelled with solid chlo...
Evaluating miniature slip ring materials and design techniques for high vacuum operatio
Vacuum test chamber to determine explosion and detonation hazards from venting of hydrogen and oxyge...
Catalysts for Aerozine-50 reforming and nitrogen tetroxide decomposition for development of rocket f...
Adverse effects of aerozine-50 leakage through propellant valves into injector manifolds exposed to ...
Moist soil introduced in vacuum chamber to determine pumping load and time require
Space storable propellant acquisition, pressurization, and tankage propulsion subsystems for Mars an...
Storable rocket propellant fuel cells - nitrogen tetraoxide and unsymmetrical dimethyl hydrazine dec...
Safety hazards accompanying use of liquid oxygen and hydrogen aboard spacecraft - cryogenic propella...
Photographic study of liquid propellant behavior in pumping from cylindrical tank during weightlessn...
Hydrazine-based bipropellant liquid propulsion system exposed to ethylene oxide and heat sterilizati...
The analyses and results of a test program to establish the effects of long term (10 years or more) ...
Data and theory pertinent to the autoignition of liquid oxygen/liquid hydrogen and liquid oxygen pro...
Detonability of gaseous hydrogen-oxygen mixtures under selected environmental condition
Strain gages, nitrocellulose effects, and mathematical models for hypervelocity launch tubes with pr...
Structure and flow properties of liquid nitrogen and liquid oxygen difluoride gelled with solid chlo...
Evaluating miniature slip ring materials and design techniques for high vacuum operatio
Vacuum test chamber to determine explosion and detonation hazards from venting of hydrogen and oxyge...
Catalysts for Aerozine-50 reforming and nitrogen tetroxide decomposition for development of rocket f...
Adverse effects of aerozine-50 leakage through propellant valves into injector manifolds exposed to ...
Moist soil introduced in vacuum chamber to determine pumping load and time require
Space storable propellant acquisition, pressurization, and tankage propulsion subsystems for Mars an...
Storable rocket propellant fuel cells - nitrogen tetraoxide and unsymmetrical dimethyl hydrazine dec...
Safety hazards accompanying use of liquid oxygen and hydrogen aboard spacecraft - cryogenic propella...
Photographic study of liquid propellant behavior in pumping from cylindrical tank during weightlessn...
Hydrazine-based bipropellant liquid propulsion system exposed to ethylene oxide and heat sterilizati...
The analyses and results of a test program to establish the effects of long term (10 years or more) ...
Data and theory pertinent to the autoignition of liquid oxygen/liquid hydrogen and liquid oxygen pro...
Detonability of gaseous hydrogen-oxygen mixtures under selected environmental condition
Strain gages, nitrocellulose effects, and mathematical models for hypervelocity launch tubes with pr...
Structure and flow properties of liquid nitrogen and liquid oxygen difluoride gelled with solid chlo...
Evaluating miniature slip ring materials and design techniques for high vacuum operatio