• DocumentCode
    2580637
  • Title

    Space structures design criteria for meteoroid-damage tolerance

  • Author

    Otani, Hiroshi

  • Author_Institution
    Nissan Motor Co. Ltd., Tokyo, Japan
  • fYear
    1991
  • fDate
    29-31 Jan 1991
  • Firstpage
    190
  • Lastpage
    195
  • Abstract
    Design criteria for the wall thickness of space structures to protect them from the expected collision impact of meteoroids during their mission periods in space are presented. The maximum expected damage by a meteoroid on a unit surface area is stochastically evaluated by applying an analytical method based on a Poisson process analysis. First, the cumulative distribution function (CDF) and mean arrival rate of meteoroids are determined from the relation between the flux number and mass of meteoroids given by NASA. Next, the probability of the maximum mass arriving at a unit surface area during a certain period of time is calculated using the Poisson process and a function of the CDF and mean arrival rate of meteoroids. To obtain the CDF for the penetration depth from a meteoroid impact, the cumulative distribution function of mass has to be replaced by that of the penetration depth. The expected penetration depth for a space structure is provided as a function of the total surface area of the structure
  • Keywords
    design engineering; failure analysis; meteoroids; probability; reliability; space vehicles; stochastic processes; NASA; Poisson process analysis; collision impact; cumulative distribution function; damage tolerance; design; mean arrival rate; meteoroids; mission periods; penetration depth; probability; space structures; stochastic processes; surface area; Distribution functions; Earthquakes; Maintenance; NASA; Process design; Protection; Risk analysis; Safety; Space missions; Space stations;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Reliability and Maintainability Symposium, 1991. Proceedings., Annual
  • Conference_Location
    Orlando, FL
  • Print_ISBN
    0-87942-661-6
  • Type

    conf

  • DOI
    10.1109/ARMS.1991.154434
  • Filename
    154434