Optimum staging principles for determining relative weights of stages of solid propellant rocket vehicle are established and relative influence of specific impulse and propellant mass fraction of various stages on performance of optimized multistage system investigated.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Optimum staging of solid-propellant rocket vehicles


    Additional title:

    Astronautica Acta


    Contributors:

    Published in:

    Publication date :

    1961


    Size :

    13 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




    Optimum staging technique for multistaged rocket vehicles

    Schurmann, E.E.H. | Engineering Index Backfile | 1957


    Solid propellant rocket motors

    Smith, E.T.B. | Engineering Index Backfile | 1957


    Solid-Propellant Rocket Engines

    A. M. Vinitskii | NTIS | 1974


    Solid propellant rocket motor

    Dowler, W. L. / Shafer, J. I. / Behm, J. W. et al. | NTRS | 1973


    Solid-Propellant Rocket Motors

    Greatrix, David R. | Springer Verlag | 2012