Mars lander deorbit trajectory sensitivity analysis for fixed flight path and communications angles at atmospheric entry, comparing with Monte Carlo simulation
Mars lander deorbit trajectory analysis
AEROSPACE SCIENCES MEETING ; 1971 ; NEW YORK, NY
01.01.1971
Aufsatz (Konferenz)
Keine Angabe
Englisch
Mars lander deorbit trajectory analysis
AIAA | 1971
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