• DocumentCode
    1890423
  • Title

    Space Transportation Main Engine reliability demonstration technique

  • Author

    Pugh, Richard L.

  • Author_Institution
    Div. of Gov. Engines & Space Propulsion, Pratt & Whitney, West Palm Beach, FL, USA
  • fYear
    1993
  • fDate
    26-28 Jan 1993
  • Firstpage
    173
  • Lastpage
    180
  • Abstract
    To satisfy the Space Transportation Main Engine (STME) reliability requirement demonstration of 99% reliability at 90% confidence, the Space Propulsion Integrated Reliability Team (SPIRT) developed a cost-efficient and effective approach using the binomial model in combination with the US Army Materiel Systems Analysis Activity (AMSAA) growth model. Using the binomial model as the base, the number of tests necessary to meet the requirement demonstration is established by assuming no failures during the demonstration test. To assist in ascertaining whether the zero failure requirement can be met during the reliability demonstration, the AMSAA growth trend will be assessed through the development testing. The results of the trend will be used to decide whether more development testing is required or the reliability demonstration can be initiated
  • Keywords
    aerospace engines; aerospace testing; reliability; AMSAA growth trend; Space Transportation Main Engine; binomial model; development testing; number of tests; reliability demonstration; zero failure requirement; Bayesian methods; Cost function; Design methodology; Engines; Propulsion; Quality function deployment; Rockets; Space technology; System testing; Transportation;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Reliability and Maintainability Symposium, 1993. Proceedings., Annual
  • Conference_Location
    Atlanta, GA
  • Print_ISBN
    0-7803-0943-X
  • Type

    conf

  • DOI
    10.1109/RAMS.1993.296858
  • Filename
    296858