Add to ORKGMission and subsystem parametric analyses to evaluate direct and orbital entry modes for soft landin...
Advanced post-Saturn earth launch vehicle design and chemonuclear propulsion system performanc
Accessible regions method for delineating generalized low thrust trajectory energy requirements and ...
Chemical propulsion for interplanetary flight and design of spacecraft for braking into orbit around...
Trajectory parameters for escaping from & braking into earth orbit utilizing single vehicle stage wi...
Integrating spacecraft/experiment payloads for solar-thermionic flight test vehicl
Evaluation results of prelaunch countdown, powered flight, and orbital phase of Saturn S-4B-501 laun...
The Skylab's Saturn Workshop mission performance is presented. Experiments were conducted to determi...
Alternative mission/system approaches to automated Mars surface sample return based on utilization o...
Earth orbital vehicle control during entry phase to simulate manned planetary entr
In-orbit performance tests of ion engines and exhaust effects on SERT 2 equipmen
Experimental static aerodynamic data for Apollo, Saturn 5 launch vehicle configuration
The environments produced by entry into Jupiter and Saturn atmospheres are summarized. Worst case de...
Saturn SA-10 range safety data, and reliability analysis of S-IV-8 and S-IV-10 stage
Modification to direct versus orbital entry for Mars mission as result of Mars environmental mode
Mission and subsystem parametric analyses to evaluate direct and orbital entry modes for soft landin...
Advanced post-Saturn earth launch vehicle design and chemonuclear propulsion system performanc
Accessible regions method for delineating generalized low thrust trajectory energy requirements and ...
Chemical propulsion for interplanetary flight and design of spacecraft for braking into orbit around...
Trajectory parameters for escaping from & braking into earth orbit utilizing single vehicle stage wi...
Integrating spacecraft/experiment payloads for solar-thermionic flight test vehicl
Evaluation results of prelaunch countdown, powered flight, and orbital phase of Saturn S-4B-501 laun...
The Skylab's Saturn Workshop mission performance is presented. Experiments were conducted to determi...
Alternative mission/system approaches to automated Mars surface sample return based on utilization o...
Earth orbital vehicle control during entry phase to simulate manned planetary entr
In-orbit performance tests of ion engines and exhaust effects on SERT 2 equipmen
Experimental static aerodynamic data for Apollo, Saturn 5 launch vehicle configuration
The environments produced by entry into Jupiter and Saturn atmospheres are summarized. Worst case de...
Saturn SA-10 range safety data, and reliability analysis of S-IV-8 and S-IV-10 stage
Modification to direct versus orbital entry for Mars mission as result of Mars environmental mode
Mission and subsystem parametric analyses to evaluate direct and orbital entry modes for soft landin...
Advanced post-Saturn earth launch vehicle design and chemonuclear propulsion system performanc
Accessible regions method for delineating generalized low thrust trajectory energy requirements and ...