Before conducting the missile composite checkout, successful performance of each individual system installed on the missile must be determined. The following is a list of the procedures used for acceptance testing of each system: Electrical system; Flight control system; Inertial guidance system; Propellant utilization system; and Propulsion system. (Author)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Factory Acceptance Testing of Missile 23F


    Publication date :

    1961


    Size :

    33 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English