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    Titel :

    AIAA-2003-5546 Trajectory Design for a Flyback Mission of a Reusable Launch Vehicle


    Beteiligte:
    Arora, R. (Autor:in) / George, J. (Autor:in) / Athnasius, X. (Autor:in) / AIAA

    Kongress:

    Conference, Atmospheric flight mechanics ; 2003 ; Austin, TX



    Erscheinungsdatum :

    2003-01-01


    Format / Umfang :

    5 pages


    Anmerkungen:

    Contains paper nos AIAA-2003-5300 to AIAA-2003-5707 with gaps



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Trajectory Design for a Flyback Mission of a Reusable Launch Vehicle

    Arora, Rajesh / George, J. / Athnasius, X. | AIAA | 2003


    AIAA-2003-5547 Trajectory Design for a Reusable Launch Vehicle Demonstrator During Re-entry Phase

    Arora, R. / Ananthasayanam, M. / AIAA | British Library Conference Proceedings | 2003


    United Trajectory Design Method for Return to Launch Site of Suborbital Reusable Launch Vehicle (AIAA 2017-2108)

    Hao, Qiao / Peng, Sun / Xinguo, Li | British Library Conference Proceedings | 2017


    Design Exploration of Aerodynamic Wing Shape for Reusable Launch Vehicle Flyback Booster

    Kazuhisa Chiba / Shigeru Obayashi / Kazuhiro Nakahashi | AIAA | 2006


    AIAA-2003-5544 Launch Condition Deviations of Reusable Launch Vehicle Simulations in Exo-Atmospheric Zoom Climbs

    Urschel, P. / Cox, T. / AIAA | British Library Conference Proceedings | 2003