United Trajectory Design Method for Return to Launch Site of Suborbital Reusable Launch Vehicle
21st AIAA International Space Planes and Hypersonics Technologies Conference
01.01.2017
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
British Library Conference Proceedings | 2017
|Concept Study of a Reusable Suborbital Launch Vehicle
AIAA | 2018
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