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Thermal Protection of Future Transatmospheric VehiclesThe field of hypersonic vehicle thermal protection is described from its beginning to the significant advancements that have been made in developing materials and systems used for thermally protecting vehicles which enter transit atmospheres. These include launch vehicles, entry and hypersonic vehicles, and planetary entry spacecraft, which as a group can be called transatmospheric vehicles which travel through the atmospheres of Earth and other planets at hypervelocities, with Mach numbers ranging from 5 to 50.
Document ID
20020064967
Acquisition Source
Ames Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Rasky, Daniel J.
(NASA Ames Research Center Moffett Field, CA United States)
Tran, Huy K.
(NASA Ames Research Center Moffett Field, CA United States)
Leiser, Daniel B.
(NASA Ames Research Center Moffett Field, CA United States)
Arnold, James O.
Date Acquired
August 20, 2013
Publication Date
January 1, 1998
Subject Category
Spacecraft Design, Testing And Performance
Funding Number(s)
PROJECT: RTOP 242-80-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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