Advantages of liquid oxygen are absolute purity and unlimited availability at relatively small cost in energy; disadvantages are those arising from impossibility of absolute isolation from heat; diagram of oxygen rocket is presented and problem of various component parts that receive particularly thorough investigation in this case but which are also often applicable to other rocket types is referred to. English translation from Schriften der Deutschen Akademie der Luftfahrtforschung v 1071 n 82 1943.


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    Titel :

    Rockets using liquid oxygen


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Tech Memo


    Beteiligte:
    Busemann, A. (Autor:in)


    Erscheinungsdatum :

    1947


    Format / Umfang :

    19 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Rockets using liquid oxygen

    Busemann, Adolf | TIBKAT | 1947


    Liquid rockets.

    Yodzis, C. W. | NTRS | 1964


    Storable liquid rockets

    STIFF, JR., R. | AIAA | 1967


    Liquid propellant rockets.

    Dipprey, D. F. | NTRS | 1972


    Liquid Propellant Rockets

    by Fouesnant | NTIS | 1968