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    Title :

    VECTOR FIELD-BASED GUIDANCE DEVELOPMENT FOR LAUNCH VEHICLE RE-ENTRY VIA ACTUATED PARAFOIL


    Contributors:

    Conference:

    IAF Space Transportation Solutions and Innovations Symposium ; 2021 ; Dubai, Stadt



    Publication date :

    2022



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :

    Classification :

    BKL:    55.60 Raumfahrttechnik




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