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    Titel :

    Design Analysis of the High-Speed Experimental Flight Test Vehicle HEXAFLY-International (AIAA 2015-3607)


    Beteiligte:

    Kongress:

    AIAA international space planes and hypersonic systems and technologies conference



    Erscheinungsdatum :

    2015-01-01


    Format / Umfang :

    22 pages



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch



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