AIAA-2003-5546 Trajectory Design for a Flyback Mission of a Reusable Launch Vehicle
Conference, Atmospheric flight mechanics ; 2003 ; Austin, TX
2003-01-01
5 pages
Contains paper nos AIAA-2003-5300 to AIAA-2003-5707 with gaps
Conference paper
English
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AIAA-2003-5547 Trajectory Design for a Reusable Launch Vehicle Demonstrator During Re-entry Phase
British Library Conference Proceedings | 2003
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