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Effect of Optical Properties on Thermal DesignWhen considering the effect of external surface optical properties, subsystems contained within the vehicle must be considered in addition to the thermal protection system. Representative subsystem temperature limits for orbital flight (long term) and entry transients (short term) are presented.
Document ID
19730024759
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Statham, C. L. (North American Rockwell Corp. Downey, CA, United States)
Tsutsui, R. T. (North American Rockwell Corp. Downey, 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. 3
Subject Category
Materials, Nonmetallic
Accession Number
73N33492
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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IDRelationTitle19730024757Collected WorksSymposium on Reusable Surface Insulation for Space Shuttle. Volume 3: Thermal Protection System Design and Optimization
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