Fig. 1 | Scientific Reports

Fig. 1

From: Starting modes of multidirectional electrodeless plasma thruster with closed ring-shaped gas discharge chamber

Fig. 1

Scheme of experimental MCEPS design: 1—propellant inlet, 2—plasma source openings, 3—toroidal magnetic field electromagnets, 4—inductor. Toroidal electromagnets are represented schematically. Arrow in inner cavity of gas discharge chamber indicates one of directions of toroidal magnetic field lines. Magnetic nozzles are not shown.

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