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Mars Sample Return Earth Entry Vehicle Design:can the Reliability Requirement Be Met by Emerging New Technologies?This proposed presentation will review past efforts and assess what emerging technologies could be used to address the reliability requirements for a Mars Sample Return Mission.
Document ID
20160011347
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Venkatapathy, Ethiraj (NASA Ames Research Center Moffett Field, CA United States)
Ellerby, Don (NASA Ames Research Center Moffett Field, CA United States)
Gage, Peter (Neerim Corp. Mountain View, CA, United States)
Mahazari, Milad (Analytical Mechanics Associates, Inc. Mountain View, CA, United States)
Peterson, Keith (Analytical Mechanics Associates, Inc. Mountain View, CA, United States)
Stackpoole, Mairead (NASA Ames Research Center Moffett Field, CA United States)
Young, Zion (NASA Ames Research Center Moffett Field, CA United States)
Date Acquired
September 19, 2016
Publication Date
June 13, 2016
Subject Category
Aerodynamics
Fluid Mechanics And Thermodynamics
Report/Patent Number
ARC-E-DAA-TN30983
Report Number: ARC-E-DAA-TN30983
Meeting Information
Meeting: International Planetary Probe Workshop (IPPW-13)
Location: Laurel, MD
Country: United States
Start Date: June 13, 2016
End Date: June 17, 2016
Sponsors: Johns Hopkins Univ.
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Ablative TPS
Multi-functional
Aeroshell

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