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Reusable surface insulations for reentry spacecraftA family of ceramic, reusable surface insulations developed for the thermal protection of reentry vehicles is discussed. Their thermal properties are summarized and their thermal capabilities are compared. The insulation requirements for the Personnel Launch System are evaluated.
Document ID
19910036966
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Chiu, S. Amanda (Sterling Software, Inc. Palo Alto, CA, United States)
Pitts, William C. (Eloret Institute Palo Alto, CA, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1991
Subject Category
Nonmetallic Materials
Report/Patent Number
AIAA PAPER 91-0695
Report Number: AIAA PAPER 91-0695
Accession Number
91A21589
Funding Number(s)
CONTRACT_GRANT: NCC2-434
Distribution Limits
Public
Copyright
Other

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