• DocumentCode
    1231402
  • Title

    Titan IIIC Ground Checkout Data Transmission System

  • Author

    Janis, James P.

  • Author_Institution
    Aerospace Corporation El Segundo, California
  • Issue
    2
  • fYear
    1965
  • fDate
    6/1/1965 12:00:00 AM
  • Firstpage
    423
  • Lastpage
    428
  • Abstract
    The increased blast area associated with the 120-inch solid rocket motors used on the Titan IIIC required locating the launch control center three and one half miles from the nearest launch complex. To transmit data over this distance, a data transmission system (DTS) with a transmission capability in excess of five miles was developed. The Titan IIIC DTS uses discrete, digital, and analog signals to monitor and control checkout and launch operations.
  • Keywords
    Aerospace control; Control systems; Costs; Data communication; Land vehicles; Open loop systems; Road vehicles; Rockets; Solids; Space vehicles;
  • fLanguage
    English
  • Journal_Title
    Aerospace, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0536-1516
  • Type

    jour

  • DOI
    10.1109/TA.1965.4319831
  • Filename
    4319831
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=1231402