Publication Date:
2019-06-27
Description:
The adaptation of the Self Evacuating Multilayer Insulation System to the space shuttle orbiter liquid hydrogen tanks was investigated. Small scale material screening tests and subscale panel tests demonstrated the potential of the insulation to withstand the anticipated 100 flight cycles. The composition of the material and the process for producing the finished insulation are described. Results of the various tests to determine the durability of the material are presented.
Keywords:
THERMODYNAMICS AND COMBUSTION
Type:
NASA-CR-121166
Format:
application/pdf
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