Add to ORKGThe Shuttle first demonstrated the capability to perform precision proximity flying in 1983 when the...
Flight simulated subsonic off-pad landing and escape maneuvers for vertically launched hypersonic gl...
Access to space is in the early stages of commercialization. Private enterprises have been making he...
Minimum fuel rendezvous guidance of powered interceptor from parking orbit to target in coplanar cir...
A study of horizontal launch concepts has been conducted. This study, jointly sponsored by the Defen...
Effect of using two separate engines in lunar lander for direct-return rendezvous with vehicl
The rendezvous targeting techniques that can be utilized to achieve autonomous guidance for deliveri...
Flight constraints and aerodynamic characteristics of hypersonic research aircraf
A study is made of the families of non-thrusting ascent trajectories during rendezvous with an orbit...
The Advanced Concepts Office at NASA's George C. Marshall Space Flight Center conducted a high-level...
Single-Stage-To-Orbit (SSTO) launch vehicles are capable of reaching orbit while being potentially f...
An investigation of a two-impulse plan for performing rendezvous on a once-a-day basis with a near-e...
The effect on performance of variations in power plant, aircraft, and rocket parameters was calculat...
An analytical and simulation study has been conducted of an automatic system for control of the term...
One of the promising launch concepts that could replace the current space shuttle launch system is a...
The Shuttle first demonstrated the capability to perform precision proximity flying in 1983 when the...
Flight simulated subsonic off-pad landing and escape maneuvers for vertically launched hypersonic gl...
Access to space is in the early stages of commercialization. Private enterprises have been making he...
Minimum fuel rendezvous guidance of powered interceptor from parking orbit to target in coplanar cir...
A study of horizontal launch concepts has been conducted. This study, jointly sponsored by the Defen...
Effect of using two separate engines in lunar lander for direct-return rendezvous with vehicl
The rendezvous targeting techniques that can be utilized to achieve autonomous guidance for deliveri...
Flight constraints and aerodynamic characteristics of hypersonic research aircraf
A study is made of the families of non-thrusting ascent trajectories during rendezvous with an orbit...
The Advanced Concepts Office at NASA's George C. Marshall Space Flight Center conducted a high-level...
Single-Stage-To-Orbit (SSTO) launch vehicles are capable of reaching orbit while being potentially f...
An investigation of a two-impulse plan for performing rendezvous on a once-a-day basis with a near-e...
The effect on performance of variations in power plant, aircraft, and rocket parameters was calculat...
An analytical and simulation study has been conducted of an automatic system for control of the term...
One of the promising launch concepts that could replace the current space shuttle launch system is a...
The Shuttle first demonstrated the capability to perform precision proximity flying in 1983 when the...
Flight simulated subsonic off-pad landing and escape maneuvers for vertically launched hypersonic gl...
Access to space is in the early stages of commercialization. Private enterprises have been making he...