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    Titel :

    DEVELOPMENT OF HIGH-BURNING-RATE HYBRID-ROCKET-FUEL FLIGHT DEMONSTRATORS



    Kongress:

    39th, Joint propulsion conference; 39th AIAA/ASME/SAE/ASEE joint propulsion conference ; 2003 ; Huntsville, AL



    Erscheinungsdatum :

    01.01.2003


    Format / Umfang :

    5196 pages


    Anmerkungen:

    Nos 2003-4404 to 2003-9731 with gaps


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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