Statistical Characteristics of Emission from Stationary Plasma Thrusters Operating with Various Propellants
Author:
Publisher
Pleiades Publishing Ltd
Subject
Space and Planetary Science,Astronomy and Astrophysics,Aerospace Engineering
Link
https://link.springer.com/content/pdf/10.1134/S0010952523700405.pdf
Reference9 articles.
1. Kim, V., Zakharchenko, V., Merkurev, D., Smirnov, P., and Shilov, E., Influence of xenon and krypton flow rates through the acceleration channel of Morozov’s stationary plasma thruster on the thrust efficiency, Plasma Phys. Rep., 2019, vol. 45, no. 1, pp. 11–20. https://doi.org/10.1134/S1063780X19010082
2. Kim, V., Merkurev, D., Shilov, E., Zakharchenko, V., and Kalyazin, V., Study of the low-power krypton-operated stationary plasma thruster plume, IOP Conf. Series: Materials Science and Engineering, Vol. 927: 13th Int. Conf. Applied Mathematics and Mechanics in the Aerospace Industry (AMMAI’2020). September 6–13, 2020, Alushta, Russia, 2020, p. 012053. https://doi.org/10.1088/1757-899X/927/1/012053
3. Plokhikh, A.P., Vazhenin, N.A., and Merkur’ev, D.V., Propellant influence on electromagnetic environment generated by stationary plasma thrusters, Kosm. Issled., 2023, vol. 61, no. 5 (in press).
4. Vazhenin, N.A., Empirical models of laws of distribution of impulse noise from stationary plasma engines, Tr. Mosk. Aviats. Inst., 2012, vol. 59, p. 15.
5. Plokhikh, A.P., Vazhenin, N.A., and Popov, G.A., Analysis of the influence of electromagnetic emission from stationary plasma thrusters on the interference immunity of the Earth–spacecraft communication channel, Cosmic Res., 2019, vol. 57, no. 5, pp. 317–324. https://doi.org/10.1134/S0010952519050071
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