Illustrated description of Reaction Motors' Model 6000C4 liquid propellant regenerative rocket plant for propelling Bell XS-1 piloted aircraft at supersonic speed; upward of 6000 lb total thrust is developed; using special injector, positive starts and stops may be made repeatedly; engine consists of four combustion cylinders plus all necessary piping, wiring, and controls, supported by single main beam assembly. (see also Flight v 51 n 1995 Mar 20 1947 p 231-2)


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    Titel :

    RMI'S rocket engine which powers supersonic XS-1


    Weitere Titelangaben:

    Aviation


    Beteiligte:
    Shesta, J. (Autor:in)

    Erschienen in:

    Aviation ; 46 , n 1 ; p 44-46


    Erscheinungsdatum :

    1947


    Format / Umfang :

    3 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    RMI'S rocket engine which powers supersonic XS-1

    Shesta, J. | Engineering Index Backfile | 1947


    Supersonic Rocket Launcher

    E. P. Lowe / R. D. Stubbs | NTIS | 1975


    Supersonic-combustion rocket

    Weber, R. J. / Franciscus, L. C. | NTRS | 1973


    Supersonic-Combustion Rocket

    R. J. Weber / L. C. Franciscus | NTIS | 1973