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Service life evaluation of rigid explosive transfer linesThis paper describes a joint Army/NASA-sponsored research program on the service life evaluation of rigid explosive transfer lines. These transfer lines are used to initiate emergency crew escape functions on a wide variety of military and NASA aircraft. The purpose of this program was to determine quantitatively the effects of service, age, and degradation on rigid explosive transfer lines to allow responsible, conservative, service life determination. More than 800 transfer lines were removed from the U.S. Army AH-1G and AH-1S, the U.S. Air Force B-1 and F-111, and the U.S. Navy F-14 aircraft for testing. The results indicated that the lines were not adversely affected by age, service, or a repeat of the thermal qualification tests on full-service lines. Extension of the service life of rigid explosive transfer lines should be considered, since considerable cost savings could be realized with no measurable decrease in system reliability.
Document ID
19830023325
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Bement, L. J.
(NASA Langley Research Center Hampton, VA, United States)
Kayser, E. G.
(NSWC Silver Spring, Md., United States)
Schimmel, M. L.
(McDonnell Aircraft Co. St. Louis, United States)
Date Acquired
September 4, 2013
Publication Date
August 1, 1983
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
L-15558
NASA-TP-2143
NAS 1.60:2143
Report Number: L-15558
Report Number: NASA-TP-2143
Report Number: NAS 1.60:2143
Accession Number
83N31596
Funding Number(s)
PROJECT: RTOP 505-42-39-69
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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