Access

    Access via TIB

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Return to Launch Site Trajectory Options for a Reusable Booster Without a Secondary Propulsion System



    Conference:

    AIAA Space Conference and Exposition ; 2009 ; Pasadena, CA



    Publication date :

    2009-01-01


    Size :

    20 pages


    Remarks:

    Includes bibliographical references and index



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :




    Return to Launch Site Trajectory Aeroheating for a Resuable Booster AIAA Paper

    Hellman, B. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2007



    Return and abort trajectory optimisation for reusable launch vehicles

    Toso, Federico / Maddock, Christie | AIAA | 2017