DocumentCode
1747140
Title
Second generation Mars landed missions
Author
Graf, James ; Thurman, Sam ; Eisen, Howard ; Rivellini, Tom ; Sabahi, Dara
Author_Institution
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
Volume
1
fYear
2001
fDate
2001
Abstract
Mars future landed missions include safe, accurate landing of payloads large enough to accomplish a sample return mission or to accommodate both a comprehensive science instrument suite and extensive in situ resource utilization payloads. In addition, the landers may be fixed (immovable) or have sufficient mobility capability to rove multiple kilometers on the surface. Accurate landing, coupled with extensive roving capability that exceeds landing error ellipses, enable “Go to” missions in which a specific, selected feature (e.g., seepage site) on the surface can be investigated with a major payload complement. This paper addresses some of the candidate missions being considered for the next-generation projects, discusses the new approaches being developed to implement safe and accurate entry, descent and landing to the Martian surface, and describes the rover technology that enables the long distance and duration surface mission
Keywords
Mars; aerospace robotics; planetary rovers; planetary surfaces; space research; space vehicle power plants; space vehicles; Mars landed missions; comprehensive science instrument suite; future landed missions; in situ resource utilization payloads; lander power generators; long duration surface mission; mobility capability; parachute descent; rover technology; safe accurate landing; sample return mission; second generation missions; surface seepage site; Energy conversion; Gears; Hardware; Instruments; Laboratories; Mars; Payloads; Planets; Propulsion; Robustness;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2001, IEEE Proceedings.
Conference_Location
Big Sky, MT
Print_ISBN
0-7803-6599-2
Type
conf
DOI
10.1109/AERO.2001.931714
Filename
931714
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