Optimal Return to Launch-Site Abort Trajectories for an HL-20 Personnel Launch Vehicle
Conference, Atmospheric flight mechanics ; 1993 ; Monterey; CA
1993-01-01
11 pages
Paper nos 93-3615 to 93-3695 with gaps bound in single vol
Conference paper
English
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RETURN-TO-LAUNCH-SITE ABORT LANDING WEATHER: IMPACT UPON LAUNCH AVAILABILITY
British Library Conference Proceedings | 2000
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