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Mars Sample Return Using Commercial Capabilities: Propulsive Entry, Descent and LandingMars Sample Return (MSR) is the highest priority science mission for the next decade as recommended by the recent Decadal Survey of Planetary Science. The objective of the study was to determine whether emerging commercial capabilities can be integrated into to such a mission. The premise of the study is that commercial capabilities can be more efficient than previously described systems, and by using fewer systems and fewer or less extensive launches, overall mission cost can be reduced. This presentation describes an EDL technique using planned upgrades to the Dragon capsule to perform a Supersonic Retropulsion Entry - Red Dragon concept. Landed Payload capability meets mission requirements for a MSR Architecture that reduces complexity.
Document ID
20140013203
Acquisition Source
Ames Research Center
Document Type
Presentation
Authors
Lemke, Lawrence G.
(NASA Ames Research Center Moffett Field, CA United States)
Gonzales, Andrew A.
(NASA Ames Research Center Moffett Field, CA United States)
Huynh, Loc C.
(Science and Technology Corp. Moffett Field, CA, United States)
Date Acquired
October 24, 2014
Publication Date
March 1, 2014
Subject Category
Lunar And Planetary Science And Exploration
Report/Patent Number
ARC-E-DAA-TN13241
Meeting Information
Meeting: 2014 IEEE Aerospace Conference
Location: Big Sky, Montana
Country: United States
Start Date: March 1, 2014
End Date: March 8, 2014
Sponsors: American Inst. of Aeronautics and Astronautics, Institute of Electrical and Electronics Engineers, PHM Society
Funding Number(s)
CONTRACT_GRANT: NNA10DF26C
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Entry
Descent and Landing
Red Dragon
Mars Sample Return
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