The LE-5A engine has been now under development for the 2nd stage of H-II launch vehicle. The LE-5A engine is an up-grade version of the LE-5 engine which is used for the H-1 launch vehicle. The LE-5A achieved 12.4 tons thrust and 452 second Isp in vacuum, and its idle mode operation was carried out successfully.


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    Titel :

    Development of LE-5A Engine and Idle Mode Operation


    Beteiligte:
    Y. Koyari (Autor:in) / A. Matsui (Autor:in) / K. Kishimoto (Autor:in) / Y. Kakuma (Autor:in) / M. Yasui (Autor:in)

    Erscheinungsdatum :

    1990


    Format / Umfang :

    7 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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