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NASA requirements and applications environments for electrical power wiringSerious problems can occur from insulation failures in the wiring harnesses of aerospace vehicles. In most recorded incidents, the failures have been identified to be the result of arc tracking, the propagation of an arc along wiring bundles through degradation of insulation. Propagation of the arc can lead to the loss of the entire wiring harness and the functions which it supports. While an extensive database of testing for arc track resistant wire insulations has been developed for aircraft applications, the counterpart requirements for spacecraft are very limited. The electrical, thermal, mechanical, chemical, and operational requirements for specification and testing of candidate wiring systems for spacecraft applications is presented.
Document ID
19930010463
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Stavnes, Mark W.
(Sverdrup Technology, Inc. Brook Park, OH, United States)
Hammoud, Ahmad N.
(Sverdrup Technology, Inc. Brook Park, OH, United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1992
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
E-7569
NAS 1.26:191064
NASA-CR-191064
Meeting Information
Meeting: Intersociety Energy Conversion Engineering Conference
Location: San Diego, CA
Country: United States
Start Date: August 3, 1992
End Date: August 7, 1992
Sponsors: AIAA, IEEE, ANS, SAE, ACS, AIChE
Accession Number
93N19652
Funding Number(s)
PROJECT: RTOP 323-57-4A
CONTRACT_GRANT: NAS3-25266
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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