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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    Titel :

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


    Beteiligte:
    M. Eymard (Autor:in) / Y. Pelipenko (Autor:in)

    Erscheinungsdatum :

    1991


    Format / Umfang :

    6 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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