Using Trajectory Optimization to Determine Design Sensitivities for Single-Stage-to-Orbit Hypersonic Vehicles
29th Joint propulsion conference ; 1993 ; Monterey; CA
01.01.1993
AIAA 93-4009
Separate paper nos 93-1752 to 93-4557 with gaps held only
Aufsatz (Konferenz)
Englisch
propulsion , AIAA , SAE , ASME , ASEE
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Single Stage to Orbit Vehicles: Issues and Sensitivities
British Library Conference Proceedings | 1994
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