NASA NTRS · 19720027094
High temperature insulation for reradiative TPS.
Abstract
This paper presents the results of a program to evaluate thermal insulations for use under the radiative TPS of a shuttle orbiter vehicle. Evaluations were made for survival under the multimission requirements of shuttle acoustic/vibration loads and thermal profiles. During the first year of the program a total of 1100 specimen-cycles were completed using metal foil packaged refractory fiber insulations.
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Hughes, T. A., King, H. M.. 1971-01-01. High temperature insulation for reradiative TPS.. https://ntrs.nasa.gov/citations/19720027094
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