• DocumentCode
    2109589
  • Title

    Emergency escape vehicles and mechanisms for space shuttles

  • Author

    Cheng, Shun-Wen

  • Volume
    4
  • fYear
    2004
  • fDate
    13-13 March 2004
  • Firstpage
    2631
  • Abstract
    This study considers emergency escape vehicles (EEV) design for Space Shuttles. The proposed EEV has the reverse Apollo-style cone configuration, contains a manned gyro-stabilized suspension rotator sphere, and has a collapsible module. Therefore, it gives astronauts a high permissible gravitational loading and survivability. The proposed EEV has high volumetric efficiency and is removable, so the Space Shuttle still can carry a large payload. The designs of the EEV system greatly extend the lifespan of the remaining space shuttle fleet indeed.
  • Keywords
    explosion protection; modules; space vehicles; Space Shuttles; collapsible module; emergency escape vehicles design; explosion protection; gravitational loading; manned gyro stabilized suspension rotator sphere; reverse Apollo style cone configuration; Aircraft; Aluminum; Earth; Equations; Explosives; Payloads; Space shuttles; Space technology; Space vehicles; Vehicle crash testing;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Aerospace Conference, 2004. Proceedings. 2004 IEEE
  • Conference_Location
    Big Sky, MT
  • ISSN
    1095-323X
  • Print_ISBN
    0-7803-8155-6
  • Type

    conf

  • DOI
    10.1109/AERO.2004.1368058
  • Filename
    1368058