System for nondissipative control of mass-flow from solid propellant gas generator is proposed; primary hypothesis of system (that propellant gas efflux can be modulated through intercession of counter-flow heat exchanger that improves heat flux from gas to solid) is studied analytically and experimentally; significant changes in burning rate can be made to occur with rams of practical design and with acceptable values of pertinent parameters; system studies incorporating models of phenomena have indicated that constant-mass flow, despite environmental temperature, and demand flow gas generators are feasible.


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    Titel :

    Control of solid propellant combustion


    Weitere Titelangaben:

    J Spacecraft Rockets


    Beteiligte:
    Mann, R.W. (Autor:in) / Marston, C.H. (Autor:in) / Stokes III, B.B. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1966


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



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