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: Abort sensing and implementation system; Azusa system; Electrical system; Flight control system; Guidance system; Propellant utilization system; Propulsion system; Range safety command system; and Telemetry system. (Author)


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    Title :

    Factory Acceptance Testing of Missile 93D


    Publication date :

    1961


    Size :

    91 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English