Data obtained from records made of reaction, fuel and liquidoxygen feed pressures, combustion chamber pressure, and duration of reaction over 25 rocket motors used in deriving three empirical rocket design formulas; with formulas as basis for rational design of liquid fuel rocket, it is shown that present development of rocket motor is already sufficient to propel meteorological rocket to altitude of 7 1/2 mi.


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    Titel :

    Design of stratosphere rocket


    Weitere Titelangaben:

    J Aeronautical Sciences


    Beteiligte:
    Africano, A. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1936


    Format / Umfang :

    4 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Rocket effluents and the stratosphere

    Bennett, R. | AIAA | 2001


    Processes in the Stratosphere Based on Rocket Sounding Data

    I. A. Khvostikov / L. A. Ryazanova | NTIS | 1965


    Processes in the stratosphere based on rocket sounding data

    Rjazanova, Lilija Aleksandrovna / Chvostikov, Ivan A. | TIBKAT | 1965