Add to ORKGExposure of assembled and fueled bipropellant liquid propulsion system to ethylene oxid
Capillary tube plugging phenomena on the 0.2-lbf thruster/valve assembly was examined. Vibration tes...
Manually operated liquid fuel control valve for Advanced Liquid Propulsion System /ALPS
Apollo service propulsion system rocket engine bipropellant valve improvement program - valve design...
In developing the highly successful bipropellant valves for the Apollo primary propulsion engines, a...
Design and performance of relief valve assembly for metabolic activity system of biological experime...
Environmental tests on designed hydraulic injector for Apollo service propulsion syste
Advanced mechanical valves and controls for liquid propellant rocket engines for space flights up to...
Basic design, component selection, and materials compatibility tests for sterilizable liquid biprope...
Environmental tests of design modifications for Apollo RCS positive expulsion tankag
An advanced design of an all metal, fast response, bipropellant, shut-off valve for use on long dura...
A monograph on valves for use with liquid rocket propellant engines is presented. The configurations...
A research program was conducted to define the level of the current technology base for reaction con...
Cold flow and hot firing test details for Apollo spacecraft ascent, descent, and service propulsion ...
Hydrazine-based bipropellant liquid propulsion system exposed to ethylene oxide and heat sterilizati...
Exposure of assembled and fueled bipropellant liquid propulsion system to ethylene oxid
Capillary tube plugging phenomena on the 0.2-lbf thruster/valve assembly was examined. Vibration tes...
Manually operated liquid fuel control valve for Advanced Liquid Propulsion System /ALPS
Apollo service propulsion system rocket engine bipropellant valve improvement program - valve design...
In developing the highly successful bipropellant valves for the Apollo primary propulsion engines, a...
Design and performance of relief valve assembly for metabolic activity system of biological experime...
Environmental tests on designed hydraulic injector for Apollo service propulsion syste
Advanced mechanical valves and controls for liquid propellant rocket engines for space flights up to...
Basic design, component selection, and materials compatibility tests for sterilizable liquid biprope...
Environmental tests of design modifications for Apollo RCS positive expulsion tankag
An advanced design of an all metal, fast response, bipropellant, shut-off valve for use on long dura...
A monograph on valves for use with liquid rocket propellant engines is presented. The configurations...
A research program was conducted to define the level of the current technology base for reaction con...
Cold flow and hot firing test details for Apollo spacecraft ascent, descent, and service propulsion ...
Hydrazine-based bipropellant liquid propulsion system exposed to ethylene oxide and heat sterilizati...
Exposure of assembled and fueled bipropellant liquid propulsion system to ethylene oxid
Capillary tube plugging phenomena on the 0.2-lbf thruster/valve assembly was examined. Vibration tes...
Manually operated liquid fuel control valve for Advanced Liquid Propulsion System /ALPS