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    Title :

    Ascent Trajectory Optimisation for a Single-Stage-to-Orbit Vehicle with Hybrid Propulsion


    Contributors:

    Conference:

    18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference



    Publication date :

    2012-01-01




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English




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