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. 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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    Titel :

    Shuttle/Agena Study. Annex a Ascent Agena Configuration


    Erscheinungsdatum :

    1972


    Format / Umfang :

    184 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch