1–13 von 13 Ergebnissen
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    100 kWe magnetoplasmadynamic thruster system design

    RUDOLPH, L. K. / KING, D. Q. | AIAA | 1984

    Thermal arcjet technology for space propulsion

    Pivirotto, T. J. / King, D. Q. | NTRS | 1985

    Electromagnetic thrusters for spacecraft prime propulsion

    Rudolph, L. K. / King, D. Q. | NTRS | 1984

    Thrust for interorbital propulsion - A question of lifetime

    Gabriel, S. B. / King, D. Q. | NTRS | 1984

    100 kWe magnetoplasmadynamic thruster system design

    Rudolph, L. K. / King, D. Q. | NTRS | 1984

    The design and operating characteristics of a 30-kW thermal arcjet engine for space propulsion

    Pivirotto, T. / King, D. Q. / Deininger, W. et al. | NTRS | 1986

    Thermal design improvements for 30kWe arcjet engine

    Deininger, William D. / Chopra, A. / King, D. Q. et al. | NTRS | 1988

    The Pegasus drive - A multi-megawatt nuclear electric propulsion system

    Coomes, E. P. / Cuta, J. M. / Webb, B. J. et al. | NTRS | 1986

    PEGASUS - A multi-megawatt nuclear electric propulsion system

    Coomes, E. P. / Cuta, J. M. / Webb, B. J. et al. | NTRS | 1986

    A comparison of arcjet plume properties to model predictions

    Cappelli, M. A. / Liebeskind, J. G. / Hanson, R. K. et al. | NTRS | 1993

    Development of a Direct Drive Hall Effect Thruster System

    Hoskins, A. / Ferguson, D. / Snyder, D. et al. | SAE Technical Papers | 2002