• DocumentCode
    1176956
  • Title

    Apollo Launch Escape Tower Electroexplosive Bolts

  • Author

    Coffman, Samuel W. ; Nussberger, Arthur A.

  • Author_Institution
    Space and Information Systems Div. North American Aviation Inc. Downey, Calif.
  • Issue
    5
  • fYear
    1966
  • Firstpage
    511
  • Lastpage
    525
  • Abstract
    Solid explosive detonation in direct contact with a metal body is examined to determine the energy transfer from latent chemical energy of an explosive into kinetic energy of the neighboring body structural members and spacecraft. Much of this is of an empirical nature since the time-dependent, three-dimensional problem involves extremely difficult analysis. Acoustic experiments were performed on a partially constructed spacecraft. A complete set of sound intensity maps was obtained.
  • Keywords
    Aerodynamics; Chemicals; Electric shock; Explosives; Fasteners; Kinetic energy; Poles and towers; Solids; Space vehicles; Temperature; Acoustic; Apollo; bolts; electroexplosive; explosive; launch; launch tower; spacecraft;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9251
  • Type

    jour

  • DOI
    10.1109/TAES.1966.4501927
  • Filename
    4501927