Publication Date:
2019-07-13
Description:
Description of a discretely oriented thread-reinforced polyurethane foam thermal insulation system for liquid hydrogen fuel tanks. The 3-D foam and glass liner composite is designed to be adhesively bonded to the inside surface of the tank wall and to be in direct contact with liquid hydrogen. All elements of this insulation composite are capable of sustaining the loads and environmental conditions imposed by testing under simulated Space Shuttle vehicle requirements at temperatures between -423 and +350 F.
Keywords:
MATERIALS, NONMETALLIC
Type:
MDAC-WD-1756
,
Society of Aerospace Material and Process Engineers, National Technical Conference on Space Shuttle Materials; Oct 05, 1971 - Oct 07, 1971; Huntsville, AL
Format:
text
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