Bonded plastic tape for lining filament-wound fiberglass cryogenic propellant tanks. [Use of fiberglass tanks results in weight savings for propellant tanks]
Technical Report
·
OSTI ID:5150948
- Research Organization:
- National Aeronautics and Space Administration, Cleveland, Ohio (USA). Lewis Research Center
- OSTI ID:
- 5150948
- Report Number(s):
- N-66-14706; NASA-TN-D-3206
- Country of Publication:
- United States
- Language:
- English
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