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NASA wiring for space applications program test resultsThe objective of this test is to examine the mechanical and electrical properties of PFPI insulation. Some of the parameters considered during the test are: AC corona (400 Hz), wire fusing time, abrasion resistance, dynamic cut through, notch propagation, and weight loss (outgassing). In addition the degradation of the samples caused by the immature manufacturing status of the PFPI materials for wiring is considered.
Document ID
19960009921
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ide, Jim (McDonnell-Douglas Aerospace Saint Louis, MO, United States)
Date Acquired
September 6, 2013
Publication Date
November 1, 1995
Publication Information
Publication: NASA. Lewis Research Center, Third NASA Workshop on Wiring for Space Applications
Subject Category
Electronics And Electrical Engineering
Accession Number
96N17087
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19960009911Collected WorksThird NASA Workshop on Wiring for Space Applications19960009911Collected WorksThird NASA Workshop on Wiring for Space Applications
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