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    Titel :

    ASCENT TRAJECTORY OPTIMISATION FOR A SINGLE-STAGE-TO-ORBIT VEHICLE WITH HYBRID PROPULSION



    Kongress:

    18th, AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference ; 2012 ; Tours, France



    Erscheinungsdatum :

    01.01.2012


    Format / Umfang :

    17 pages


    Anmerkungen:

    Includes bibliographical references and index



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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