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Aerothermal Analysis and Thermal Protection System (TPS) Design of the Mars Sample Retrieval Lander (SRL) ConceptThis poster provides a glimpse of the aerothermal analysis and TPS design work for the Mars Sample Retrieval Lander (SRL), part of the Mars Sample Return (MSR) architecture.
Document ID
20190028643
Acquisition Source
Ames Research Center
Document Type
Poster
External Source(s)
ippw2019.uk
Authors
Muppidi, S. (Analytical Mechanics Associates, Inc. Moffett Field, CA, United States)
Mcguire, M. K. (NASA Ames Research Center Moffett Field, CA, United States)
Kinney, D. J. (NASA Ames Research Center Moffett Field, CA, United States)
Saunders, D. A. (Analytical Mechanics Associates, Inc. Moffett Field, CA, United States)
Bensassi, K. (Analytical Mechanics Associates, Inc. Moffett Field, CA, United States)
Date Acquired
August 1, 2019
Publication Date
July 8, 2019
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
ARC-E-DAA-TN70488
Meeting Information
Meeting: International Planetary Probe Workshop 2019 (IPPW 2019)
Location: Oxford
Country: United Kingdom
Start Date: July 8, 2019
End Date: July 12, 2019
Sponsors: University of Oxford
Funding Number(s)
CONTRACT_GRANT: NNA15BB15C
Distribution Limits
Public
Copyright
Public Use Permitted.

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