• DocumentCode
    2290543
  • Title

    Application of test effectiveness in spacecraft testing

  • Author

    Lang, Paul ; Card, Michael ; Saalwaechter, Susie ; Godkin, Todd

  • Author_Institution
    SRS Technol., Arlington, VA, USA
  • fYear
    1995
  • fDate
    16-19 Jan 1995
  • Firstpage
    486
  • Lastpage
    495
  • Abstract
    This article summarizes test design practices of selected NASA Centers and prime contractors as they are used to evaluate the performance and reliability of space mission payloads. It also reports the use of previous relevant test experience to avoid risk in the design of future spacecraft and enhance test programs. Test effectiveness (TE) is defined as the ability of a test to accurately emulate the expected mission environment, and reliably detect failure causing defects before launch. These twin objectives determine the value of a test program relative to project funding
  • Keywords
    aerospace testing; design engineering; failure analysis; reliability; space vehicles; NASA; contractors; design; failure; mission environment; performance; reliability; space mission payloads; spacecraft testing; test design practices; test effectiveness; Aerospace engineering; Aerospace testing; Isolation technology; NASA; Payloads; Qualifications; Reliability engineering; Space technology; Space vehicles; System testing;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Reliability and Maintainability Symposium, 1995. Proceedings., Annual
  • Conference_Location
    Washington, DC
  • ISSN
    0149-144X
  • Print_ISBN
    0-7803-2470-6
  • Type

    conf

  • DOI
    10.1109/RAMS.1995.513289
  • Filename
    513289