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Entry, Descent and Landing Systems Analysis: Exploration Class Simulation Overview and ResultsNASA senior management commissioned the Entry, Descent and Landing Systems Analysis (EDL-SA) Study in 2008 to identify and roadmap the Entry, Descent and Landing (EDL) technology investments that the agency needed to make in order to successfully land large payloads at Mars for both robotic and exploration or human-scale missions. The year one exploration class mission activity considered technologies capable of delivering a 40-mt payload. This paper provides an overview of the exploration class mission study, including technologies considered, models developed and initial simulation results from the EDL-SA year one effort.
Document ID
20100030602
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
DwyerCianciolo, Alicia M.
(NASA Langley Research Center Hampton, VA, United States)
Davis, Jody L.
(NASA Langley Research Center Hampton, VA, United States)
Shidner, Jeremy D.
(Analytical Mechanics Associates, Inc. Hampton, VA, United States)
Powell, Richard W.
(Analytical Mechanics Associates, Inc. Hampton, VA, United States)
Date Acquired
August 25, 2013
Publication Date
August 2, 2010
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NF1676L-10123
Report Number: NF1676L-10123
Meeting Information
Meeting: AIAA/AAS Astrodynamics Specialist Conference
Location: Toronto
Country: Canada
Start Date: August 2, 2010
End Date: August 5, 2010
Sponsors: American Inst. of Aeronautics and Astronautics, American Astronomical Society
Funding Number(s)
WBS: WBS 811540.16.09.07
Distribution Limits
Public
Copyright
Public Use Permitted.
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