• 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