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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    Title :

    Trajectory Optimization Using XGESOP: Ariane V GTO Trajectory Optimization


    Contributors:

    Publication date :

    1994


    Size :

    52 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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