1–12 von 12 Ergebnissen
|

    Description of arcjet facilities at BPD

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

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

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

    Development of a 1N, radiatively cooled arcjet

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

    Emission spectroscopy of 15 kWe arcjet plumes

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

    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

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

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

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

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

    Nuclear reactor power for an electrically powered orbital transfer vehicle

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

    Velocity measurements in the plume of an arcjet engine

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