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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    Title :

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


    Contributors:
    J. Borromee (author) / D. Thevenot (author) / H. Dederra (author) / A. Faure (author)

    Publication date :

    1988


    Size :

    10 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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