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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Global Optimization of Air Breathing Launch Vehicle Trajectories


    Contributors:
    F. Martel (author)

    Publication date :

    1990


    Size :

    9 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Small Air Breathing Launch Vehicle

    L. R. Jackson / W. J. Small / J. P. Weidner et al. | NTIS | 1978