Proposed plasma rocket, described in report, generates hybrid exhaust plume comprising annular layer of relatively cool neutral gas around plasma core. Plasma and gas intermix, providing gradual radial transition between the two. Amount of gas injected adjusted to control propulsive efficiency; relatively cool gas boundary layer at surface of nozzle insulates nozzle from high plasma temperature.


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    Titel :

    Plasma Rocket With Hybrid Exhaust Plume


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    01.09.1987



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Rocket exhaust plume dimensions

    DYNER, H. B. | AIAA | 1969


    Rocket exhaust plume phenomenology

    Simmons, Frederick S. | TIBKAT | 2000



    Small rocket exhaust plume data

    Chirivella, J. E. / Moynihan, P. I. / Simon, W. | NTRS | 1972


    JANNAF handbook rocket exhaust plume technology / Chemical Propulsion Information Agency; [JANNAF Exhaust Plume Technology Subcommittee] ; Chapter 3: Rocket exhaust plume radiation

    Chemical Propulsion Information Agency / USA, Joint Army Navy NASA Air Force Exhaust Plume Technology Subcommittee | TIBKAT | 1980