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Space Shuttle statusHardware considerations and the orbital flight test program of the Space Shuttle are discussed, including reference to the Space Shuttle main engine, payload bay doors, TV cameras for flight inspection, and launch crew escape schemes. Particular attention is given to the thermal protection system consisting of 32,000 tiles composed of approximately 3% pure silica fibers and 97% air, which has a design requirement of keeping the basic aluminum skin below 350 F for a surface temperature of 2700 F.
Document ID
19800043215
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Slayton, D. K.
(NASA Johnson Space Center Houston, Tex., United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1979
Subject Category
Space Transportation
Accession Number
80A27385
Distribution Limits
Public
Copyright
Other

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