International Journal of Aerospace Engineering / 2013 / Article / Fig 1

Research Article

Experimental Investigations of a Krypton Stationary Plasma Thruster

Figure 1

Schematic view of the ATON A-3 SPT: (1) gas distributor, (2) anode, (3) cathode-compensator, (4) magnetic coils, (5) buffer volume, (6) magnetic circuit, and (7) dielectric channel;  mm.
686132.fig.001

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