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TPS and Entry System Technologies for Future Mars and Titan Exploration
The purpose of this white paper is to provide an overview to the NRC Decadal Survey Mars and Ocean Worlds Sub-Panels on thermal protection system (TPS) technologies required for future Mars and Titan exploration missions. It considers the capability of heritage TPS technology used by previous Mars and Titan missions. A prime conclusion is that there are important advances regarding the availability of forebody TPS therefore, we recommend that NASA invest in a cross-cutting technology program that focuses on development and sustainment of relevant TPS materials, entry systems, test facilities, design tools, and flight instrumentation.
Document ID
20205006951
Acquisition Source
Ames Research Center
Document Type
White Paper
Authors
Robin Beck
(Ames Research Center Mountain View, California, United States)
Milad Mahzari
(Ames Research Center Mountain View, California, United States)
Helen Hwang
(Ames Research Center Mountain View, California, United States)
Mairead Stackpoole
(Ames Research Center Mountain View, California, United States)
Ethiraj Venkatapathy
(Ames Research Center Mountain View, California, United States)
Donald Ellerby
(Ames Research Center Mountain View, California, United States)
Todd White
(Ames Research Center Mountain View, California, United States)
Alan Cassell
(Ames Research Center Mountain View, California, United States)
Cooper Snapp
(Johnson Space Center Houston, Texas, United States)
Date Acquired
August 28, 2020
Publication Date
September 1, 2020
Subject Category
Engineering (General)
Funding Number(s)
WBS: 971200.02.01.02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
NASA Peer Committee
Keywords
Thermal protection systems
Mars exploration
Titan exploration
Ablative materials
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