Many disadvantages inherent in conventional booster sustainer systems can be eliminated by designing desired thrust program into single solid propellant engine of type under development; configurations include tandem chamber configuration, one or two propellants in one chamber, and one partitioned chamber with one propellant in each of partitioned sections.


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    Titel :

    Why not dual-thrust engines?


    Weitere Titelangaben:

    Astronautics


    Beteiligte:
    Newman, R.S. (Autor:in)

    Erschienen in:

    Astronautics ; 3 , n 3 ; p 26-28 + 48-49


    Erscheinungsdatum :

    1958


    Format / Umfang :

    2 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




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