Abstract—
A scheme of a spacecraft thruster based on pulsed plasma railgun with capillary–porous electrodes is proposed. Electrodes of this kind are renewable and do not degrade while their lifetime is limited by the stored amount of the filler metal of the capillary–porous electrode. Operating regimes in which capillary–porous electrodes are efficient are found. In these regimes, the proposed railgun construction can yield the thrust of several newtons and specific impulse of several tens of km/s. Li, Sn, and Ga can be used as filler metals of capillary–porous electrodes with porous mats made from molybdenum or tungsten.
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ACKNOWLEDGMENTS
The authors are grateful to M.N. Kazeev for useful discussions.
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Martynenko, Y.V., Nagel’, M.Y. Plasma Railgun with Capillary–Porous Electrodes. Plasma Phys. Rep. 47, 362–368 (2021). https://doi.org/10.1134/S1063780X21040073
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DOI: https://doi.org/10.1134/S1063780X21040073