LAUNCH VEHICLE AND MISSILE (LV/M) TECHNOLOGY - Abort Separation of Launch Escape System Using Aerodynamic Interference (TN)
AIAA journal ; 51 , 1
2013
Aufsatz (Zeitschrift)
Englisch
NASA Crew Exploration Vehicle and Launch Abort Tower Aerodynamic Separation Characteristics
British Library Conference Proceedings | 2009
|NTRS | 2019
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