The design criteria and methodology of the Ariane 5 main stage are reviewed. The thrust chamber, main injector, and hydrogen pump are described. Differences between the cryogenic tanks of Ariane 5 and Ariane 4 are explained. The simulation and analysis programs are indicated.


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    Titel :

    Technology and Design Method Evolution of Cryogenic Propulsion Systems: Example of the Main Ariane 5 Stage


    Beteiligte:
    J. Borromee (Autor:in) / D. Thevenot (Autor:in) / H. Dederra (Autor:in) / A. Faure (Autor:in)

    Erscheinungsdatum :

    1988


    Format / Umfang :

    10 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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