NASA NTRS · 19870000227
Reusable High-Temperature/Cryogenic Foam-Insulation System
Abstract
Flightweight insulation withstands wide temperture cycling. Reusable insulation system for cryogenic containment vessels withstands repeated exposures to thermal environments that span ranges from cryogenic-fluid temperature {-425oF (-254oC)} to maximum use temperature of containment-tank material {+400oF (+204oC)}. System designed for use with high-speed flight vehicles.
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Davis, Randall C., Taylor, Allan H., Jackson, L. Robert, Mcauliffe, Patrick. 1987-05-01. Reusable High-Temperature/Cryogenic Foam-Insulation System. https://ntrs.nasa.gov/citations/19870000227
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