Add to ORKGPerformance capability and vehicle dynamics of Saturn 5 launch vehicle for two engine out malfunctions for Saturn S-1C stag
Kinesthetic versus pivot thrust vector control for lunar flying vehicle with flying characteristics ...
A preliminary spacecraft servicing demonstration plan is prepared which leads to a fully verified op...
Technology was identified which will enable application of hybrid propulsion to manned and unmanned ...
Apollo 9 evasive maneuver after command service module/lunar module ejection from Saturn S-4B stage ...
Stage separation dynamics of parallel staged reusable launch vehicles at Mach 3 and
Preflight analysis of LUMINARY 1B DAP simulation and performance testing for Apollo Mission H
Low thrust chemical (hydrogen-oxygen) propulsion systems configured specifically for low acceleratio...
Possible storable propellant configurations and program plans are evaluated for the space tug. Alter...
Lightning Attach Point tests were conducted for the space shuttle launch configuration (Orbiter, Ext...
Feasibility study summary of remote manipulator for satellite repair and maintenance in orbi
Ground effects experiments and large/small-tunnel interference studies were carried out on a model w...
The design, fabrication, and initial testing of a rocket engine turbopump (TPA) for the delivery of ...
The results are presented of an investigation to determine the capability of a monopropellant hydraz...
The ascent opeational flight profile for the space transportation system 1 flight is designed (1) to...
Deviations from the traditional spacecraft data systems were studied. A data system architecture was...
Kinesthetic versus pivot thrust vector control for lunar flying vehicle with flying characteristics ...
A preliminary spacecraft servicing demonstration plan is prepared which leads to a fully verified op...
Technology was identified which will enable application of hybrid propulsion to manned and unmanned ...
Apollo 9 evasive maneuver after command service module/lunar module ejection from Saturn S-4B stage ...
Stage separation dynamics of parallel staged reusable launch vehicles at Mach 3 and
Preflight analysis of LUMINARY 1B DAP simulation and performance testing for Apollo Mission H
Low thrust chemical (hydrogen-oxygen) propulsion systems configured specifically for low acceleratio...
Possible storable propellant configurations and program plans are evaluated for the space tug. Alter...
Lightning Attach Point tests were conducted for the space shuttle launch configuration (Orbiter, Ext...
Feasibility study summary of remote manipulator for satellite repair and maintenance in orbi
Ground effects experiments and large/small-tunnel interference studies were carried out on a model w...
The design, fabrication, and initial testing of a rocket engine turbopump (TPA) for the delivery of ...
The results are presented of an investigation to determine the capability of a monopropellant hydraz...
The ascent opeational flight profile for the space transportation system 1 flight is designed (1) to...
Deviations from the traditional spacecraft data systems were studied. A data system architecture was...
Kinesthetic versus pivot thrust vector control for lunar flying vehicle with flying characteristics ...
A preliminary spacecraft servicing demonstration plan is prepared which leads to a fully verified op...
Technology was identified which will enable application of hybrid propulsion to manned and unmanned ...