• DocumentCode
    2203150
  • Title

    Study on Vulnerability Model of Spacecraft Impacting by Orbital Debris

  • Author

    LIU, Chunmei ; FENG, Shunshan ; ZHANG, Xurong

  • Author_Institution
    State Key Lab. of Explosion Sci. & Technol., Beijing Inst. of Technol., Beijing, China
  • fYear
    2008
  • fDate
    20-22 Dec. 2008
  • Firstpage
    1067
  • Lastpage
    1070
  • Abstract
    The spacecraft was studied. Spacecraft vulnerability was analyzed in some aspects as environment, representative structure, aviation theory, damage principle and existence speciality. Then the destruction types were advanced on debris against double plates. The damage types included local perforation and avulsion. And the respective lethality model was put forward. At last the damage probability was obtained when one fragment impacts the double boards by hypervelocity. It is a certain reference and important reality signification, that the vulnerability analysis and lethality mathematical model of spacecraft are researched, to strengthen our space defense ability.
  • Keywords
    aerospace safety; probability; space debris; space vehicles; aviation theory; damage probability; destruction type; hypervelocity; lethality model; orbital debris; representative structure; spacecraft existence speciality; spacecraft vulnerability model; work environment; Aerodynamics; Aircraft manufacture; Airplanes; Control systems; Engines; Gravity; Satellites; Space debris; Space vehicles; Vehicle detection; damage probability; orbital debris; spacecraft; vulnerability mathematics model;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Advanced Computer Theory and Engineering, 2008. ICACTE '08. International Conference on
  • Conference_Location
    Phuket
  • Print_ISBN
    978-0-7695-3489-3
  • Type

    conf

  • DOI
    10.1109/ICACTE.2008.103
  • Filename
    4737121