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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    Title :

    RMI'S rocket engine which powers supersonic XS-1


    Additional title:

    Aviation


    Contributors:
    Shesta, J. (author)

    Published in:

    Aviation ; 46 , n 1


    Publication date :

    1947


    Size :

    3 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




    RMI'S rocket engine which powers supersonic XS-1

    Shesta, J. | Engineering Index Backfile | 1947



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    Supersonic Rocket Launcher

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    Supersonic-combustion rocket

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