DocumentCode
1228429
Title
Ablestar Reliability and Launch Site Testing
Author
Doshay, I. ; Tusa, J.A.
Author_Institution
Space-General Corporation El Monte, California
Volume
1
Issue
2
fYear
1963
Firstpage
1227
Lastpage
1235
Abstract
A study was made to determine the influence of tests made at the factory, at the launch site and on the launch pad to establish flight readiness and system reliability. Based on data from tests on the Ablestar Stage vehicle, relationships of locational failure incidence as well as functional characteristics are developed. Failure rate levels are shown to be highly dependent on the conditions or stresses at the three different locations. It is also determined that failure rates are increasing with prolonged periods of system test. Conclusions are drawn that field tests should be minimized and only performed for purposes of multi-stage operational integrity.
Keywords
Aerospace testing; Delay effects; Engines; Performance evaluation; Production facilities; Reliability; Satellites; Stress; System testing; Vehicles;
fLanguage
English
Journal_Title
Aerospace, IEEE Transactions on
Publisher
ieee
ISSN
0536-1516
Type
jour
DOI
10.1109/TA.1963.4319500
Filename
4319500
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