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Thermal support for scale supportThe thermal design work completed for the Thermal Protection System (TPS) of the Space Shuttle System (TPS) of the space shuttle vehicle was documented. This work was divided into three phases, the first two of which reported in previous documents. About 22 separate tasks were completed in phase III, such as: hot gas facility (HGF) support, guarded tank support, shuttle external tank (ET) thermal design handbook support, etc.
Document ID
19760012131
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Dean, W. G. (Lockheed Missiles and Space Co. Huntsville, AL, United States)
Date Acquired
September 3, 2013
Publication Date
January 1, 1976
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-CR-144185
LMSC-HREC-TR-D496704
Report Number: NASA-CR-144185
Report Number: LMSC-HREC-TR-D496704
Accession Number
76N19219
Funding Number(s)
CONTRACT_GRANT: NAS8-25569
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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