Publication Date:
2014-09-09
Description:
When 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.
Keywords:
MATERIALS, NONMETALLIC
Type:
NASA. Ames Res. Center Symp. on Reusable Surface Insulation for Space Shuttle, Vol. 3; p 965-980
Format:
text
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