First order objectives of the flight included obtaining data on the re-entry vehicle impact location for the statistical determination of CEP, the evaluation of the flight control system performance, the evaluation of the inertial guidance system performance and accuracy and the evaluation of the performance of the acoustica PU system. (Author)


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    Title :

    WS 107A-1Flight Test Working Group Flight Test Report Atlas Missile 25E 2 October 1961 AMR Range Test Number 1252, Astronautics Test Number P1-503-00-25


    Publication date :

    1961


    Size :

    88 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English