1–41 von 41 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

    Influence of driving power on directional stability of vehicles

    Deininger, W. | Engineering Index Backfile | 1965

    Velocity measurements in the plume of an arcjet engine

    PIVIROTTO, T. / DEININGER, W. | AIAA | 1987

    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

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

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

    Development testing of a 1kW class arcjet thruster

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

    Long duration test of a 30-kW class thermal arcjet engine

    PIVIROTTO, T. / KING, D. / DEININGER, W. | AIAA | 1987

      Long duration test of a 30-kW class thermal arcjet engine

      PIVIROTTO, T. / KING, D. / DEININGER, W. | AIAA | 1987

    Cathode erosion tests for 30 kW arcjets

    DEININGER, W. / CHOPRA, A. / GOODFELLOW, K. | AIAA | 1989

    Development of a 1N, radiatively cooled arcjet

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

    Effect of cathode configuration on 30 kWe arcjet electrical characteristics

    CHOPRA, A. / DEININGER, W. / KING, D. | AIAA | 1989

    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

    Emission spectroscopy of 15 kWe arcjet plumes

    TOSTI, E. / DEININGER, W. / MAZZACURATI, V. et al. | AIAA | 1990

    Low power arcjet system requirements definition for North-South station keeping

    DEININGER, W. / ATTILI, M. / VULPIANI, M. et al. | 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 Conference Proceedings | 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 Online Contents | 1997

    Integration of an Arcjet System on the Modular STB Lightsat Platform

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

    The Vacuum Facilities at the FIAT AVIO Electric Propulsion Laboratory

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

    Description of arcjet facilities at BPD

    CRUCIANI, G. / TOSTI, E. / GLOGOWSKI, M. et al. | AIAA | 1990

    Comparison of low power arcjet operation at BDP and Centrospazio

    DEININGER, W. / CRUCIANI, G. / GLOGOWSKI, M. et al. | AIAA | 1992

    A review of low power arcjet PCU development and testing

    Deininger, W. / Di Stefano, R. / Parisi, G. et al. | AIAA | 1994

    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

    Low cost access to Mars-Mars micromissions spacecraft

    Deininger, W. D. / Epstein, K. W. / Eterno, J. S. et al. | British Library Conference Proceedings | 2003

    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

    Description of the Green Propellant Infusion Mission (GPIM) mission system

    Deininger, W. D. / Gilmore, C. P. / Hale, M. J. et al. | IEEE | 2014

    Space technology three: mission overview and spacecraft concept description

    Deininger, W. D. / Noecker, M. C. / Wiemer, D. J. et al. | British Library Conference Proceedings | 2003

    Scale Effects On Solid Propellant MPD Thruster Performance

    Paccani, G. / Petrucci, L. / Deininger, W. D. et al. | British Library Conference Proceedings | 1998