A study aimed at showing the possible development of solid propellant boosters is presented. Two examples are used: low stage boosters (the Ariane 5 P230) and upper stage boosters (MAGE engine). The three main parameters driving the development and improvement of launch vehicles such as Ariane 5 are functional safety (automatic and manned flight); competitiveness with other launch means; and performance.


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    Title :

    Evolution de la Conception des Propulseurs a Propergol Solide (Development of Solid Propellant Booster)


    Contributors:
    M. Eymard (author) / Y. Pelipenko (author)

    Publication date :

    1991


    Size :

    6 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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