The primary purposes of the flight were to obtain data for determining the performance of the Propellant Utilization System and to evaluate the Inertial Guidance System Performance. (Author)


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    Title :

    WS 107A-1Flight Test Working Group, Flight Test Report, Atlas Missile 32E


    Publication date :

    1961


    Size :

    69 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English