Performance of air-breathing launch vehicles is investigated. A simple set of 'alpha-beta' relations are used at the core of some simple trajectory, propulsion and structural models, to obtain qualitative information about possible design directions. Only single-stage-to-orbit vehicles are discussed for reasons of brevity. Optimum vehicle types are suggested. For example, optimum air-breathing termination velocity emerges for a class of vehicles attempting to enter the high-hypersonic regime. Some propulsion systems and strategies are discussed. It is concluded that the 'alpha-beta' relations are useful and that with careful optimisation, performance gains over all-rocket SSTO vehicles could be reached.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Optimum directions for air-breathing launch vehicle design


    Weitere Titelangaben:

    Optimale Entwicklungsrichtungen fuer die Konzipierung von luftansaugenden Raumfahrzeugen


    Beteiligte:

    Erschienen in:

    AIAA-Papers ; Jul ; 1-9


    Erscheinungsdatum :

    1987


    Format / Umfang :

    9 Seiten, 4 Bilder, 4 Tabellen, 16 Quellen


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch






    Small Air Breathing Launch Vehicle

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