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Development and Sizing of the Mars 2020 Thermal Protection SystemThe Mars 2020 entry vehicle successfully delivered the Perseverance rover to the Martian surface on 18 February 2021. The entry vehicle aeroshell was shielded from aerodynamic heating with a thermal protection system (TPS) made of three different ablative materials. This paper provides an overview of the methodology and assumptions employed for the thermal sizing and design of the Mars 2020 aeroshell TPS. The sizing results demonstrate that the as-built thicknesses of the TPS materials were sufficient to withstand the predicted aerothermal environments without exceeding temperature limits of the underlying aeroshell structure. This paper also provides an overview of the ground testing performed in NASA arc jet facilities to verify the performance of flight lot TPS materials. Finally, temperature data returned by thermocouples embedded in the flight vehicle TPS are compared with predictions by the thermal response models used in pre-flight TPS sizing.
Document ID
20220009403
Acquisition Source
Ames Research Center
Document Type
Presentation
Authors
Milad Mahzari
(Ames Research Center Mountain View, California, United States)
Robin Beck
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
Helen Hwang
(Ames Research Center Mountain View, California, United States)
Josh Monk
(Ames Research Center Mountain View, California, United States)
Jonathan Morgan
(Ames Research Center Mountain View, California, United States)
Joseph Williams
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
Karl Edquist
(Langley Research Center Hampton, Virginia, United States)
Date Acquired
June 16, 2022
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: AIAA Aviation Forum
Location: Chicago, IL
Country: US
Start Date: June 27, 2022
End Date: July 1, 2022
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 971200.02.01.02
CONTRACT_GRANT: NNA15BB15C
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Technical Management
Keywords
Mars2020
Thermal Protection System
EDL
Heatshield
PICA
SLA-561V
Acusil-II
Arcjet Testing
TPS Sizing
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