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Volumn 2, Issue , 2002, Pages 559-574
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Mars sample return, a concept point design by Team-X (JPL's advanced project design team)
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Author keywords
[No Author keywords available]
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Indexed keywords
AERODYNAMIC CONTROL;
EARTH ENTRY VEHICLES;
FLIGHT SYSTEM DESIGN;
MARS ORBIT INSERTION;
MARS SAMPLE RETURN MISSIONS;
PROJECT DESIGN TEAMS;
TECHNOLOGY ADVANCES;
TECHNOLOGY DEVELOPMENT;
LAUNCH VEHICLES;
MARTIAN SURFACE ANALYSIS;
DESIGN;
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EID: 84879387347
PISSN: 1095323X
EISSN: None
Source Type: Conference Proceeding
DOI: 10.1109/AERO.2002.1035567 Document Type: Conference Paper |
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Times cited : (21)
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References (0)
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