Background and features of system in which tanks are pressurized by means of solid propellant charge, and combined with combustion chamber to form single package in which propellants are self-igniting; principal characteristics such as resistance to environmental conditions; design problems and possible developments with regard to selection of propellants, materials, burning time, ignition and combustion, and safety; possible applications related to missiles, aircraft, and space projects.


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    Titel :

    Packaged liquid rocket motors


    Weitere Titelangaben:

    Roy Aeronautical Soc -- J


    Beteiligte:
    Neat, W.N. (Autor:in) / Page, K.G. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1962


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




    Liquid propellant rocket motors

    Diplock, B.R. / Lofts, D.L. / Grimston, R.A. | Engineering Index Backfile | 1953


    Microfabricated Liquid Rocket Motors

    Epstein, Alan H. / Joppin, C. / Kerrebrock, J. L. et al. | NTRS | 2003