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Follow-on cable coupling lightning test, volume 1A redesigned solid rocket motor test article was subjected to simulated lightning strikes. This test was performed to evaluate the effects of lightning strike to the redesigned motor and Space Transportation System. The purpose of the test was to evaluate the performance of systems tunnel design changes when subjected to the lightning discharges. The goal of the design changes was to reduce lightning induced coupling to cables within the systems tunnel. The test article was subjected to several different amounts and kinds of discharges. Changes in coupling levels detected during the tests are recorded. The dominant mode of coupling appears to be caused by the diffusion of the magnetic fields through the system tunnel covers. The results from bond strap integrity testing showed that 16 of 18 bond straps survived. Design change evaluations showed that coupling reduction ranged from 0 to 36 decibels for each type of cable. The type of cable has less effect on coupling than does strike location and strike levels. Recommendations for design changes are made.
Document ID
19910018878
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Danforth, Richard
(Thiokol Corp. Brigham City, UT, United States)
Date Acquired
September 6, 2013
Publication Date
October 31, 1990
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-CR-184123
PUBL-91230
TWR-60187-VOL-1
NAS 1.26:184123
Report Number: NASA-CR-184123
Report Number: PUBL-91230
Report Number: TWR-60187-VOL-1
Report Number: NAS 1.26:184123
Accession Number
91N28192
Funding Number(s)
CONTRACT_GRANT: NAS8-30490
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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