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
Link To Document :
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