Abstract
The fundamental principles allowing control of the ionization and acceleration layer position and thickness in the discharge of a stationary plasma thruster (SPT) determining ion flows to the discharge chamber walls and the corresponding energy losses and wall erosion rate are considered in this work. These principles have allowed the development of modern SPTs with a long life life that have already been successfully used for many years in space technology. Some of these principles were formulated earlier on the basis of available data and were not fully verified from the physical point of view. To date some new investigations have been carried out. Using them, some new principles are formulated and the earlier ones are corrected in this paper. These principles can be used in the processes of new thruster development.
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REFERENCES
A. I. Morozov, Plasma Phys. Rep. 29, 235 (2003).
K. N. Kozubskii, V. M. Murashko, Yu. P. Rylov, Yu. V. Trifonov, V. P. Khodnenko, V. P. Kim, G. A. Popov, and V. A. Obukhov, Plasma Phys. Rep. 29, 251 (2003).
R. Hofer, H. Kamhavi, D. Herman, et al., in Proc. 30th Int. Symposium on Space Technology and Science, 34th Int. Electric Propulsion Conference, and 6th Nano-Satellite Symposium (Kobe, July 4–10, 2015), Paper IEPC-2015-186 /ISTS-2015-b-186.
V. P. Kim, Tech. Phys. 60, 362 (2015).
V. P. Kim, Plasma Phys. Rep. 43, 486 (2017).
V. P. Kim and V. K. Abgaryan, Tech. Phys. Lett. 43, 948 (2017).
A. M. Bishaev and V. P. Kim, Zh. Tekh. Fiz. 48, 1853 (1978).
A. M. Bishaev and V. Kim, in Plasma Sources and Accelerators. Collection of Scientific Papers (Kharkov Aviation Institute, Kharkov, 1981), No. 5, p. 3 [in Russian].
V. Kim, K. N. Kozubsky, V. M. Murashko, and A. V. Semenkin, in Proc. 30th Int. Electric Propulsion Conference (Florence, September 17–20, 2007), Paper IEPC-2007-142.
B. A. Arkhipov, A. M. Bishaev, V. M. Gavryushin, Yu. M. Gorbachev, N. A. Maslennikov, V. P. Kim, K. N. Kozubskii, A. I. Morozov, and D. D. Sevruk, RF Patent No. 2030134 (1995).
Yu. V. Esipchuk and G. N. Tilinin, Zh. Tekh. Fiz. 46, 718 (1976).
G. Goduti, A. Lazurenko, S. Mazoufre, M. Dudeck, and A. Bouchoule, in Proc. 30th Int. Electric Propulsion Conference (Florence, September 17–20, 2007), Paper IEPC-2007-143.
D. A. Tomilin and O. A. Gorshkov, in Proc. 32nd Int. Electric Propulsion Conference (Wiesbaden, September 11–15, 2011), Paper IEPC-2011-023.
N. V. Belan, V. P. Kim, A. I. Oranskii, and V. B. Tikhonov, Stationary Plasma Thrusters. Student’s Book (Kharkov Aviation Institute, Kharkov, 1989) [in Russian].
O. A. Mitrofanova and R. Yu. Gnizdor, in Proc. 33rd Int. Electric Propulsion Conference, George Washington University, Washington, DC, October 6–10, 2013 (Washington, DC, 2013), Paper IEPC-2013-51.
S. D. Grishin, V. S. Erofeev, and A. V. Zharinov, Plasma Accelerators, Ed. by L. A. Artsimovich (Mashinostroenie, Moscow, 1973), p. 54 [in Russian].
A. Shagayda, O. Gorshkov, and D. Tomilin, in Proc. 32nd Int. Electric Propulsion Conference (Wiesbaden, September 11–15, 2011), Paper IEPC-2011-025.
B. A. Arhipov, A. S. Bober, R. Y. Gnizdor, K. N. Kozubsky, A. I. Koryakin, N. A. Maslennikov, and S. Yu. Pridannikov, in Proc. 24th Int. Electric Propulsion Conference (Moscow, 1995), Paper IEPC-1995-039.
Cho Shinatora, H. Watanabe, K. Kubota, Sh. Iihara, K. Fuchigami, K. Uematsu, and I. Funaki, in Proc. 30th Int. Symposium on Space Technology and Science, 34th Int. Electric Propulsion Conference, and 6th Nano-Satellite Symposium (Kobe, July 4–10, 2015), Paper IEPC-2015-251/ISTS-2015-b-251.
M. Yu. Potapenko and V. V. Gopanchuk, in Proc. 32nd Int. Electric Propulsion Conference (Wiesbaden, September 11–15, 2011), Paper IEPC-2011-042.
A. Arkhipov, S. Baranov, A. Bishayev, V. Kim, G. Popov, D. Merkuriev, A. Pogorelov, and P. Tsygankov, in Proc. 30th Int. Symposium on Space Technology and Science, 34th Int. Electric Propulsion Conference, and 6th Nano-Satellite Symposium (Kobe, July 4–10, 2015), Paper IEPC-2015-247/ISTS- 2015-b-247.
M. Sekerak, R. Hofer, J. Polk, and I. Mikellides, in Proc. 30th Int. Symposium on Space Technology and Science, 34th Int. Electric Propulsion Conference, and 6th Nano-Satellite Symposium (Kobe, July 4–10, 2015), Paper IEPC-2015-155/ISTS-2015-b-155.
ACKNOWLEDGMENTS
This work was supported by the Ministry of Education and Science of the Russian Federation within the state assignment to the Moscow Aviation Institute under the agreement on granting subsidy no. 14.577.21.0231 of September 29, 2016 (unique identifier PNIER-RFMEF157716X0231).
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Kim, V.P., Gnizdor, R.Y., Grdlichko, D.P. et al. Fundamental Principles Employed for Ionization and Acceleration Layer Control in the Discharge of a Stationary Plasma Thruster. J. Surf. Investig. 12, 1237–1247 (2018). https://doi.org/10.1134/S1027451018050610
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DOI: https://doi.org/10.1134/S1027451018050610