Abstract On the base of the simplified analytical model for the bimetallic shell of the combustion chamber of the reusable liquid-propellant rocket engine, the analysis of the loading of connectors between the shell walls and the accumulation of inelastic deformations in the inner wall material was carried out. The results obtained can be used for evaluation of the maximal number of engine operation cycles.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Estimation of the Combustion Chamber Shell Working Capacity for the Reusable Liquid-Propellant Rocket Engine


    Beteiligte:
    Zarubin, V. S. (Autor:in) / Zimin, V. N. (Autor:in) / Kuvyrkin, G. N. (Autor:in)

    Erschienen in:

    Russian Aeronautics ; 61 , 3 ; 425-433


    Erscheinungsdatum :

    2018-07-01


    Format / Umfang :

    9 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





    Simulation of liquid propellant rocket engine combustion instabilities

    VENTRICE, M. / FANG, J. / PURDY, K. | AIAA | 1979


    Design and Analysis for Reusable Liquid Rocket Engine Chamber

    Chen, Tao / Yang, Jinhui / Jin, Ping et al. | AIAA | 2013


    Simulation of Liquid Propellant Rocket Engine Combustion InsEabilities

    M. B. Ventrice / J.C. Fang / K.R. Purdy | AIAA | 1979