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    Titel :

    Two Stage to Orbit Conceptual Vehicle Designs using the SABRE Engine (AIAA 2016-5320)


    Beteiligte:

    Kongress:

    Space (conference)



    Erscheinungsdatum :

    2016-01-01


    Format / Umfang :

    16 pages



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch



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