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Flexible Composite-Material Pressure VesselA proposed lightweight pressure vessel would be made of a composite of high-tenacity continuous fibers and a flexible matrix material. The flexibility of this pressure vessel would render it (1) compactly stowable for transport and (2) more able to withstand impacts, relative to lightweight pressure vessels made of rigid composite materials. The vessel would be designed as a structural shell wherein the fibers would be predominantly bias-oriented, the orientations being optimized to make the fibers bear the tensile loads in the structure. Such efficient use of tension-bearing fibers would minimize or eliminate the need for stitching and fill (weft) fibers for strength. The vessel could be fabricated by techniques adapted from filament winding of prior composite-material vessels, perhaps in conjunction with the use of dry film adhesives. In addition to the high-bias main-body substructure described above, the vessel would include a low-bias end substructure to complete coverage and react peak loads. Axial elements would be overlaid to contain damage and to control fiber orientation around side openings. Fiber ring structures would be used as interfaces for connection to ancillary hardware.
Document ID
20110024160
Acquisition Source
Johnson Space Center
Document Type
Other - NASA Tech Brief
Authors
Brown, Glen
(Vertigo, Inc. CA, United States)
Haggard, Roy
(Vertigo, Inc. CA, United States)
Harris, Paul A.
(Vertigo, Inc. CA, United States)
Date Acquired
August 25, 2013
Publication Date
June 1, 2003
Publication Information
Publication: NASA Tech Briefs, June 2003
Subject Category
Man/System Technology And Life Support
Report/Patent Number
MSC-23020
Distribution Limits
Public
Copyright
Public Use Permitted.
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