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Sustained load behavior of graphite/epoxy metal-lined pressure vessels for long-life space applicationsTests were performed on candidate graphite yarns for the overwraps to be used on the Space Station Freedom's pressure vessels. The objective was to determine the performance and ranking of these overwraps to ensure that sustained loads would not be a problem during their 30-yr life in space. Tests were conducted at high stress levels for short time periods on subscale composite bottles. The average delivered fiber stresses were determined from the measured burst pressures via SCI analysis that accounts for both geometry and the properties of the resin and yarn.
Document ID
19890059613
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Babel, H. W.
(McDonnell-Douglas Astronautics Co. Huntington Beach, CA, United States)
Vickers, B. D.
(McDonnell Douglas Space Systems Co. Huntington Beach, CA, United States)
Thomas, D. A.
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
August 14, 2013
Publication Date
July 1, 1989
Subject Category
Composite Materials
Report/Patent Number
AIAA PAPER 89-2644
Accession Number
89A46984
Distribution Limits
Public
Copyright
Other

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