Studies of the power of high-frequency losses in the toroidal resonator of a prototype of the high-frequency ion thruster
https://doi.org/10.25206/2588-0373-2025-9-3-92-100
EDN: TUYNLK
Abstract
The authors present a prototype of an accelerator micro thruster for a small spacecraft with a maximum power consumption of 5 W. The design is demonstrated and the main structural elements are described. Moreover, the paper also presents vacuum calorimetric studies of the power of high-frequency losses in the volume of a toroidal resonator for various working fields: air, helium, carbon dioxide, nitrogen, argon and water vapor. Due to the joint measurement of the main frequencies of the oscillator with calorimetric studies, the electrical capacitances of the oscillating circuit are obtained. With prototype 4–4.8 power consumption the calculated values of accelerating alternating voltages are 199.65–287.9 V for various gases. The measured power of high-frequency losses is 0.088–0.183 W, which is no more than 4 % of the total power consumption.
About the Authors
I. S. VavilovRussian Federation
VAVILOV Igor Sergeevich, Candidate of Technical Sciences, Associate Professor of the Aircraft and Rocket Building Department
Omsk, Mira Ave., 11, 644050
AuthorID (RCSI): 518332
AuthorID (SCOPUS): 56610211900
ResearcherID: B-2634-2014
K. I. Zharikov
Russian Federation
ZHARIKOV Konstantin Igorevich, Candidate of Technical Sciences, Associate Professor of the Aircraft and Rocket Building Department
Omsk, Mira Ave., 11, 644050
AuthorID (SCOPUS): 57192074889
ResearcherID: E-9087-2014
P. S. Yachmenev
Russian Federation
YACHMENEV Pavel Sergeevich, Assistant, Postgraduate of the Aircraft and Rocket Building Department
Omsk, Mira Ave., 11, 644050
AuthorID (SCOPUS): 57193405041
ResearcherID: P-5381-2016
I. A. Kuzmenko
Russian Federation
KUZMENKO Irina Anatolievna, Senior Lecturer of the Aircraft and Rocket Building Department
Omsk, Mira Ave., 11, 644050
AuthorID (SCOPUS): 686832
I. V. Volod’kov
Russian Federation
VOLOD’KOV Ilya Vladislavovich, Master’s Student of the РКм-231 group of the Aircraft and Rocket Building Department
Omsk, Mira Ave., 11, 644050
References
1. Vavilov I. S., Yachmenev P. S., Fedyanin V. V. [et al.]. Eksperimental'nye issledovaniya prototipa ionnogo dvigatelya vremyaproletnym metodom [Experimental study of ion thruster by time-of-flight method]. Dinamika sistem, mekhanizmov i mashin. Dynamics of Systems, Mechanisms and Machines. 2023. Vol. 11, no. 2. P. 30–36. DOI: 10.25206/2310-9793-2023-11-2-30-36. EDN: KFJUEQ. (In Russ.).
2. Jarrige J., Elias P. Q., Packan D. [et al.]. Characterization of a coaxial ECR plasma thruster. 44th AIAA Plasmadynamics and Lasers Conference. 2013. P. 1–9. DOI: 10.2514/6.2013-2628.
3. Vialis T., Jarrige J., Aanesland A. [et al.]. Direct thrust measurement of an electron cyclotron resonance plasma thruster. Journal of Propulsion and Power. 2018. Vol. 34, no. 5. P. 1–11. DOI: 10.2514/1.B37036.
4. Charles C. Plasmas for spacecraft propulsion. Journal of Physics D: Applied Physics. 2009. Vol. 42, no. 16. P. 163001. DOI: 10.1088/0022-3727/42/16/163001.
5. Squire J., Olsen C., Cassady L. [et al.]. Improved efficiency and throttling range of the VX-200 magnetoplasma thruster. Journal of Propulsion and Power. 2014. Vol. 30. P. 123–132. DOI: 10.2514/1.B34801.
6. Squire J., Carter M., Diaz F. [et al.]. VASIMR® spaceflight engine system mass study and scaling with power. The 33st International Electric Propulsion Conference. USA, 2013.
7. Chen F. F. Physics of helicon discharges. Physics of Plasmas — PHYS PLASMAS. 1996. Vol. 3, no. 5. P. 1783–1793. DOI: 10.1063/1.871697.
8. Geller R. Electron cyclotron resonance ion sources and ECR plasmas. Routledge, 1996. 434 p. ISBN 9780203758663. DOI: 10.1201/9780203758663.
9. Vavilov I. S., Yachmenev P. S., Fedyanin V. V. [et al.]. Opredeleniye moshchnosti SVCh/VCh-poter’ v toroidal’nom rezonatore uskoritel’nogo ionnogo dvigatelya po ego spektru chastot [Determination of the power of the microwave/HF losses in the toroidal resonator of the accelerator ion thruster by its frequency spectrum]. Dinamika sistem, mekhanizmov i mashin. Dynamics of Systems, Mechanisms and Machines. 2023. Vol. 11, no. 2. P. 21–29. DOI: 10.25206/2310-9793-2023-11-2-21-29. EDN: PTANKK. (In Russ.).
10. Orlov S. I. Raschet i konstruirovaniye koaksial’nykh rezonatorov [Calculation and construction of coaxial resonators]. Moscow, 1970. 256 p. (In Russ.).
Review
For citations:
Vavilov I.S., Zharikov K.I., Yachmenev P.S., Kuzmenko I.A., Volod’kov I.V. Studies of the power of high-frequency losses in the toroidal resonator of a prototype of the high-frequency ion thruster. Omsk Scientific Bulletin. Series Aviation-Rocket and Power Engineering. 2025;9(3):92-100. (In Russ.) https://doi.org/10.25206/2588-0373-2025-9-3-92-100. EDN: TUYNLK
JATS XML

















