Development and validation of purged thermal protection systems for liquid hydrogen fuel tanks of hypersonic vehicles
An economical, lightweight, safe, efficient, reliable, and reusable insulation system was developed for hypersonic cruise vehicle hydrogen fuel tanks. Results indicate that, a nitrogen purged, layered insulation system with nonpermeable closed-cell insulation next to the cryogenic tank and a high service temperature fibrous insulation surrounding it, is potentially an attractive solution to the insulation problem. For the postulated hypersonic flight the average unit weight of the purged insulation system (including insulation, condensate and fuel boil off) is 6.31 kg/sq m (1.29 psf). Limited cyclic tests of large specimens of closed cell polymethacrylimide foam indicate it will withstand the expected thermal cycle.
- Research Organization:
- Bell Aerospace Co., Buffalo, N.Y. (USA)
- DOE Contract Number:
- NAS1-10969
- OSTI ID:
- 5322751
- Report Number(s):
- N-77-25455; NASA-CR-2829; REPT-8653-950001
- Country of Publication:
- United States
- Language:
- English
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