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Mass loss of shuttle space suit orthofabric under simulated ionospheric atomic oxygen bombardmentMany polymeric materials used for thermal protection and insulation on spacecraft degrade significantly under prolonged bombardment by ionospheric atomic oxygen. The covering fabric of the multilayered shuttle space suit is composed of a loose weave of GORE-TEX fibers, Nomex and Kevlar-29, which are all polymeric materials. The complete evaluation of suit fabric degradation from ionospheric atomic oxygen is of importance in reevaluating suit lifetime and inspection procedures. The mass loss and visible physical changes of each test sample was determined. Kapton control samples and data from previous asher and flight tests were used to scale the results to reflect ionospheric conditions at about 220 km altitude. It is predicted that the orthofabric loses mass in the ionosphere at a rate of about 66% of the original orthofabric mass/yr. The outer layer of the two-layer orthofabric test samples shows few easily visible signs of degradation, even when observed at 440X. It is concluded that the orthofabric could suffer significant loss of performance after much less than a year of total exposure time, while the degradation might be undetectable in post flight visual examinations of space suits.
Document ID
19860004430
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Miller, W. L.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
November 1, 1985
Subject Category
Man/System Technology And Life Support
Report/Patent Number
NAS 1.15:87149
E-2777
NASA-TM-87149
Accession Number
86N13899
Funding Number(s)
PROJECT: RTOP 506-41-4C
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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