• DocumentCode
    1175978
  • Title

    Electroexplosive Devices in Aerospace Vehicle Systems

  • Author

    Moses, Sidney A.

  • Author_Institution
    Douglas Aircraft Company, Inc. Missile & Space Systems Division
  • Issue
    4
  • fYear
    1966
  • fDate
    7/1/1966 12:00:00 AM
  • Firstpage
    51
  • Lastpage
    56
  • Abstract
    Reasons for using electroexplosive devices in aerospace vehicles are given. A number of different electroexplosive devices are illustrated and their uses are described. The explosive materials used in these devices are discussed in two classes: propellants and high explosives. Methods for controlling deflagration or detonation to achieve desired effects are discussed. Construction of a typical electroexplosive cartridge is described, with special reference to the bridgewire-explosive system. A ??bridgewire equation?? is suggested for determining the functioning characteristics of the system. The method of determining the reliability of these ??one-shot?? items is compared to that used for devices which may be operated for a number of cycles. Safety of handling electroexplosive devices is discussed along with a few common-sense rules for accident prevention.
  • Keywords
    Aerospace materials; Aircraft; Circuits; Electric shock; Electron tubes; Explosives; Missiles; Propellants; Pulse amplifiers; Vehicles;
  • fLanguage
    English
  • Journal_Title
    Aerospace and Electronic Systems, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9251
  • Type

    jour

  • DOI
    10.1109/TAES.1966.4501821
  • Filename
    4501821