Being considered are the selection problems of rational thermodynamic parameters and control laws for hydrogen and hydrogen-oxyen aero-turbo-rocket (ATR) engines designed for horizontal take-off and landing Single-Stage-to-Orbit (SSTO) vehicles acceleration up to Mach 6. Three types of ATR-engines were studied: gas generator, expander, gas generator with H2 preheating. Computation allows for thermodynamic features of cryogenic-fuelled engines, operating within a wideflight speed envelope. Construction materials performance corresponded to world practice 2005-2010 years forecast. Relative payload mass was used for estimation of different type ATR-engines effectiveness for SSTO.


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    Titel :

    Rational schemes and performances of the ATR-engines


    Weitere Titelangaben:

    Kriterien für die Entwicklung und Leistung von ATR-Raketentriebwerken (Aero-Turbo-Rocket)


    Beteiligte:
    Lanshin, A.I. (Autor:in) / Dulopov, N.P. (Autor:in)

    Erschienen in:

    SAE-Papers ; Apr ; 1-8


    Erscheinungsdatum :

    1990


    Format / Umfang :

    8 Seiten, 10 Bilder, 10 Quellen



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Rational Schemes and Performances of the ATR-Engines

    Lanshin, A. I. / Dulepov, N. P. | SAE Technical Papers | 1990




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    Dennison, E. S. | SAE Technical Papers | 1935


    Analysis of performances of some diesel propelling engines

    Robb, A.M. | Engineering Index Backfile | 1937