In this report the Faculty of Aerospace Engineering (Faulty LR), TU-Delft, investigates the necessity of space launcher trajectory optimization for the conceptual design of airplane-like space launchers. For this purpose, the Faculty LR acquired in 1994 the highly advanced, German-developed trajectory optimization tool referred to as XGESOP. In this memorandum the capabilities of XGESOP will be demonstrated.


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    Titel :

    Trajectory Optimization Using XGESOP: Ariane V GTO Trajectory Optimization


    Beteiligte:
    A. G. M. Maree (Autor:in)

    Erscheinungsdatum :

    1994


    Format / Umfang :

    52 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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