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Silica RSI entry simulation testsSimulated reentry heating of the all-silica surface insulation material under a variety of conditions including arc jet and radiant lamp facilities for up to 100 simulated flight cycles has demonstrated consistent thermal performance capability. Consistent predictability along with demonstrated coating integrity and dimensional stability to 1645 K validates the earlier selection of the all-silica material for the RSI application.
Document ID
19730024749
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Banas, R. P.
(Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Donaldson, J. O.
(Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Jue, J.
(Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Date Acquired
August 7, 2013
Publication Date
September 1, 1973
Publication Information
Publication: NASA. Ames Res. Center Symp. on Reusable Surface Insulation for Space Shuttle, Vol. 2
Subject Category
Aerodynamics
Accession Number
73N33482
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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