An analytical study of mode transition in the integral ramjet-rocket class of propulsion system was conducted. A baseline design was selected and used for analysis. The several factors affecting the engine aerothermodynamic performance during mode transition were evaluated. A quantitative evaluation method was established to aid in design of future engines of this class. Specific developmental recommendations are made. (Author)


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    Titel :

    Mode Transition in Integral Ramjet Rocket Propulsion Systems


    Beteiligte:
    W. G. Beecroft (Autor:in) / R. E. Petersen (Autor:in)

    Erscheinungsdatum :

    1972


    Format / Umfang :

    65 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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