A trajectory global optimization method for single stage to orbit (SSTO) air breathing launch vehicle is presented. This method was involved in STS 2000 Aerospatiale studies to compare various air breathing candidate solutions, assess their performances, and contribute to the definition of an optimized SSTO global design.


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    Titel :

    Global Optimization of Air Breathing Launch Vehicle Trajectories


    Beteiligte:
    F. Martel (Autor:in)

    Erscheinungsdatum :

    1990


    Format / Umfang :

    9 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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