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Unlined Reuseable Filament Wound Composite Cryogenic Tank TestingAn unlined reusable filament wound composite cryogenic tank was tested at the Marshall Space Flight Center using LH2 cryogen and pressurization to 320 psig. The tank was fabricated by Phillips Laboratory and Wilson Composite Group, Inc., using an EnTec five-axis filament winder and sand mandrels. The material used was IM7/977-2 (graphite/epoxy).
Document ID
19990019399
Acquisition Source
Marshall Space Flight Center
Document Type
Technical Memorandum (TM)
Authors
Murphy, A. W. (NASA Marshall Space Flight Center Huntsville, AL United States)
Lake, R. E. (NASA Marshall Space Flight Center Huntsville, AL United States)
Wilkerson, C. (NASA Marshall Space Flight Center Huntsville, AL United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1999
Subject Category
Composite Materials
Report/Patent Number
NAS 1.15:209039
M-909
NASA/TM-1999-209039
Report Number: NAS 1.15:209039
Report Number: M-909
Report Number: NASA/TM-1999-209039
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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