Results of analytical investigations to determine stability and steering effectiveness during high speed slide-out are presented for spacecraft equipped with main gear skids and nose wheel; it is shown that steering control during slideout is necessary, and that sufficient steering capability may be developed for landing on 150 ft wide runway; method of nose wheel steering is employed which eliminates possibility of ground looping due to oversteering and provides for advantageous use of aerodynamic side force in steering. (recd 4/1/69) (31539)


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    Titel :

    Stability and steering control during slideout of skid-equipped horizontally landing spacecraft


    Weitere Titelangaben:

    AIAA/ASME, Struc Dynamics and Mater Conf


    Beteiligte:
    Feld, D.J. (Autor:in)

    Kongress:

    9th Conference of AIAA/ASME on Structures, Structural Dynamics and Materials ; 1968 Landing



    Erscheinungsdatum :

    1968


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




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