Details are presented on the Agena rocket vehicle description, vehicle interfaces, environmental constraints and test requirements, software programs, and ground support equipment. The basic design concept for the Ascent Agena is identified as optimization of reliability, flexibility, performance capabilities, and economy through the use of tested and flight-proven hardware. The development history of the Agenas A, B, and D is outlined and space applications are described.


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    Title :

    Shuttle/Agena study. Annex A: Ascent agena configuration


    Publication date :

    1972-02-15


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :