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: Azusa system; Electrical system; Flight control system; Inertial guidance system; Instrumentation Beacon system; Propellant utilization system; Propulsion system; Range safety command system; and Telemetry system.


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    Title :

    Factory Acceptance Testing of Missile 40E


    Publication date :

    1961


    Size :

    65 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English