1–20 von 26 Ergebnissen
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    Advanced propulsion system options for geostationary satellites

    Deininger, W. | AIAA | 1994

      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

    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 testing of a 1kW class arcjet thruster

    CRUCIANI, G. / DEININGER, W. | AIAA | 1992

    A 300-hour endurance test of an arcjet thruster at 1 kW

    CRUCIANI, G. / DEININGER, W. | AIAA | 1993

    Performance comparisons of low-power arcjets

    Deininger, W. D. / Cruciani, G. / Glogowski, M. J. | AIAA | 1995

    Integration of an Arcjet System on the Modular STB Lightsat Platform

    Deininger, W. D. / De Lorenzo, G. / Attili, M. | British Library Online Contents | 1997

    Integration of an Arcjet System on the Modular STB Lightsat Platform

    Deininger, W. D. / De Lorenzo, G. / Attili, M. | British Library Conference Proceedings | 1997

    The Vacuum Facilities at the FIAT AVIO Electric Propulsion Laboratory

    De Lorenzo, G. / Deininger, W. D. / Magnanimi, M. | British Library Online Contents | 1997

    Hollow-Cathode Source Generates Plasma

    Deininger, W. D. / Aston, G. / Pless, L. C. | NTRS | 1989

    Plasma Source for Charge Control

    Aston, G. / Pless, L. C. / Deininger, W. D. | NTRS | 1986

    The Vacuum Facilities at the FIAT AVIO Electric Propulsion Laboratory

    De Lorenzo, G. / Deininger, W. D. / Magnanimi, M. | British Library Conference Proceedings | 1997

    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

    Development and Testing of a New Thermal Protection Material for Reentry Vehicles

    Santovincenzo, A. / Deininger, W. / La Motta, G. et al. | British Library Conference Proceedings | 1995

    A Modular Satellite Bus for the "Romolo & Remo" Dual Lightsat Magnetosphere Analysis Mission

    Attili, M. / Balduccini, M. / Deininger, W. D. et al. | British Library Conference Proceedings | 1995

    Experimental Analysis of a Solid Propellant MPD Thruster with Different Anode Radii

    Paccani, G. / Petrucci, L. / Deininger, W. D. et al. | British Library Conference Proceedings | 1999