The performance of a magnetoplasmadynamic arc thruster, in the 600 to 2,100 seconds specific impulse range, was improved by locating its cathode in the exhaust beam downstream of the anode and main propellant injection point.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Magneto-plasma-dynamic arc thruster


    Contributors:

    Publication date :

    1973-05-29


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




    Magneto-Plasma-Dynamic Arc Thruster

    J. A. Burkhart | NTIS | 1973


    Magneto Plasma Dynamic Arc Thruster

    J. A. Burkhart | NTIS | 1971


    OPTICAL INVESTIGATIONS ON A MAGNETO-PLASMA-DYNAMIC THRUSTER

    Borghi, C. A. / Carraro, M. R. / Cristofolini, A. et al. | British Library Conference Proceedings | 2003


    Numerical Analysis of a Magneto-Plasma-Dynamic Thruster

    Cristofolini, A. / Ghedini, R. / Borghi, C.A. | AIAA | 2002


    Optical Diagnostics in a Magneto-Plasma-Dynamic Thruster

    Borghi, Carlo / Cristofolini, A / Ghedini, R | AIAA | 2002