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System definition study of deployable, non-metallic space structuresThe state of the art for nonmetallic materials and fabrication techniques suitable for future space structures are summarized. Typical subsystems and systems of interest to the space community that are reviewed include: (1) inflatable/rigidized space hangar; (2) flexible/storable acoustic barrier; (3) deployable fabric bulkhead in a space habitat; (4) extendible tunnel for soft docking; (5) deployable space recovery/re-entry systems for personnel or materials; (6) a manned habitat for a space station; (7) storage enclosures external to the space station habitat; (8) attachable work stations; and (9) safe haven structures. Performance parameters examined include micrometeoroid protection; leakage rate prediction and control; rigidization of flexible structures in the space environment; flammability and offgassing; lifetime for nonmetallic materials; crack propagation prevention; and the effects of atomic oxygen and space debris. An expandable airlock for shuttle flight experiments and potential tethered experiments from shuttle are discussed.
Document ID
19840020818
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Stimler, F. J.
(Goodyear Aerospace Corp. Akron, OH, United States)
Date Acquired
September 4, 2013
Publication Date
June 1, 1984
Subject Category
Launch Vehicles And Space Vehicles
Report/Patent Number
GAC-19-1615
NAS 1.26:171090
NASA-CR-171090
Report Number: GAC-19-1615
Report Number: NAS 1.26:171090
Report Number: NASA-CR-171090
Accession Number
84N28887
Funding Number(s)
CONTRACT_GRANT: NAS8-35498
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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