To alleviate earth landing loads on Apollo command module, configuration was considered by North American Inc consisting of command module and heat shield; command module and heat shield are connected by arrangement of active (oleo) and passive (crushable core) struts; equations of motion describing response of vehicle for impact landings are developed for simulation of operational analog computer; structural and inertial properties of vehicle are represented by normal modes of vibration in conjunction with conventional longitudinal dynamic-stability of freedom; simulation techniques and problems.


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    Titel :

    Apollo earth landing simulation


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Blackburn, C.L. (Autor:in) / Gongaware, R.W. (Autor:in)

    Kongress:

    SAE Meeting ; 1964 Landing



    Erscheinungsdatum :

    1964


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Apollo Earth Landing Simulation

    Blackburn, Charles L. / Gongaware, Robert W. | SAE Technical Papers | 1964





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    Lowry, C. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2011