1–9 von 9 Ergebnissen
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    Development of an arcjet nuclear electric propulsion system for a 1993 flight demonstration

    DEININGER, W. / VONDRA, R. | AIAA | 1986

    Electric propulsion for constellation deployment and spacecraft maneuvering

    DEININGER, W. / VONDRA, R. | AIAA | 1988

    A review of nuclear electric propulsion spacecraft system concepts

    DEININGER, W. / NOCK, K. | AIAA | 1990

    Development of a 1N, radiatively cooled arcjet

    CRUCIANI, G. / DEININGER, W. / PETAGNA, C. | AIAA | 1990

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

    PIVIROTTO, T. / KING, D. / DEININGER, W. et al. | AIAA | 1986

      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

    Nuclear reactor power for an electrically powered orbital transfer vehicle

    JAFFE, L. / BEATTY, R. / BHANDARI, P. et al. | AIAA | 1987

      Nuclear reactor power for an electrically powered orbital transfer vehicle

      Jaffe, L. / Beatty, R. / Bhandari, P. et al. | NTRS | 1987

    Nuclear reactor power as applied to a space-based radar mission

    Jaffe, L. / Beatty, R. / Bhandari, P. et al. | NTRS | 1988

      Nuclear reactor power as applied to a space-based radar mission

      Jaffe, L. / Fujita, T. / Beatty, R. et al. | NTRS | 1988

    Advanced Propulsion System Options for Geostationary Satellites

    Deininger, W. D. / American Institute of Aeronautics and Astronautics / Society of Automotive Engineers et al. | British Library Conference Proceedings | 1994