Comparison of performance capabilities and growth history of hybrids with other forms of chemical propulsion systems is presented showing advantages of hybrid engine concept; feasibility of most outstanding features which include high impulse, start/stop operation, modulated thrust, and insensitivity to temperature pressure, has been demonstrated; efficient throttling up to thrust levels of 10 to 1 is practical; knowledge of combustion process has been established to point where grain and engines can be designed to achieve efficient performance.


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    Titel :

    Recent developments and current status of hybrid rocket propulsion


    Weitere Titelangaben:

    J Spacecraft Rockets


    Beteiligte:
    Ordahl, D.D. (Autor:in) / Rains, W.A. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1965


    Format / Umfang :

    4 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




    Hybrid rocket propulsion

    Holzman, Allen L. | NTRS | 1993


    Hybrid Rocket Propulsion

    A. L. Holzman | NTIS | 1993


    Hybrid rocket propulsion

    Barrere, M. / Moutet, A. | TIBKAT | 1964