Научная электронная библиотека ULRICH'S Periodicals Directory

Сибирский государственный университет
науки и технологий имени академика М.Ф. Решетнева

Сибирский аэрокосмический журнал
ISSN 2712-8970 (Print) ISSN 2782-5760 (on-line)

Сведения об образовательной организации

UDK 629.78: 629.036 Doi: 10.31772/2587-6066-2018-19-3-489-496
ON THE CONCEPT OF ALL ELECTRIC PROPULSION SPACECRAFT
Yu. M. Yermoshkin*, D. V. Volkov, E. N. Yakimov
JSC “Academician M. F. Reshetnev “Information Satellite Systems” 52, Lenina Str., Zheleznogorsk, Krasnoyarsk Region, 662972, Russian Federation *E-mail: erm@iss-reshetnev.ru
Over the past several years the concept of the so-called “all electric propulsion spacecraft” has gained popularity among both customers and developers of geostationary (GEO) spacecraft; this issue is being actively discussed. The main advantages of the concept are the following: decreasing the mass of spacecraft and increasing its economic efficiency by means of pair orbital injection. There are some illustrative cases of implementation of this concept by American, European and Russian companies. However, specialists interpret the content of the concept in different ways. That causes the problems connected to the development of the conceptual design of spacecraft. It is therefore very important to consider the concept in more detail, to compare various points of view in order to form understanding reflecting its essence the most accurately. At the same time, on the basis of the available examples, it would be feasible to analyze the advantages and disadvantages of this concept in comparison with other approaches to the construction of propulsion system of spacecraft. In the article we offer to interpret the concept as “All electric propulsion spacecraft”. This interpretation allows to understand its content unambiguously by the specialists of both Russian and Western Technical Schools. We offer to define “All electric propulsion spacecraft” as an apparatus that does not have in its composition an apogee engine unit that is chemically fuelled. It has to execute manoeuvres on geostationary orbit raising, orbit correction and momentum wheel unloading by electrical propulsion only. We have shown that with the existing level of excellence of the equipment this concept does not have any advantages over the concept of separate propulsion subsystems for the correction and orientation by total mass as well as by the level of reliability.
Keywords: all electric propulsion spacecraft, apogee thruster, propulsion subsystem, electric propulsion engine, orbit raising.
References

1. Popov G., Kim V., Murashko V. et al Electric Propulsion Subsystem Development and Application in Russia. 3rd International Conference “Spacecraft Propulsion”. Cannes, France, October 10–13, 2000, 9 p.

2. Chien K., Hart S., Tighe W. et al. L-3 Communications ETI Electric Propulsion Overview. 29th International Electric Propulsion Conference. IEPC-2005-315. Princeton University. Oct. 31–Nov. 4, 2005, 16 p.

3. Lev D., Myers R.V., Lemmer K. M. et al.. The Technological and Commercial Expansion of Electric Propulsion in the Past 24 Years. 35th Electric Propulsion Conference. IEPC-2017-242. Georgia Institute of Technology. USA, October 8–12, 2017, 18 p.

4. De Tata M., Frigor P., Beekmans S. et al. SGEO Electric Propulsion Subsystem Development Status and Future Opportunities. 33rd International Electric Propulsion Conference. IEPC-2013-144. The George Washington University, USA, October 6–10, 2013, 11 p.

5. Casaregola C. Electric Propulsion for Station Keeping and Electric Orbit Raising on Eutelsat Platform. 34th International Electric Propulsion Conference, IEPC-2015-97. Kobe-Hyogo, Japan, July 4–10, 2015, 6 p.

6. Vnukov A. A., Rvacheva E. I. [Backgrounds and trends of all-electric propulsion geostationary satellites creation for the operation in geostationary orbit]. Vestnik SibGAU. 2014, No. 4(56), P. 140–146 (In Russ.).

7. Volkov D. V., Yermoshkin Y. M., Yakimov Y. N. [The application of propulsion subsystems of experimental design bureau “Fakel” on spacecraft developed by JSC “ISS”]. Elektroreaktivnyie sistemy OKB “Fakel” [Electric propulsion of EDB “Fakel”]. Kaliningrad, 2010, Р. 113–119.

8. Lovtsov A. S., Tomilin D. A., Muravlev V. A. Development of High-Voltage Hall Effect Thrusters at Keldysh Research Centre. 68th International Astronautical Congress (IAC), Adelaide, Australia, September 25–29, 2017, 5 p.

9. Yermoshkin Y. M., Zhitnik Y. N, Ladygin A. P. [Development of the storage and feeding equipment for the spacecraft electric propulsion subsystems at JSC “ISS”]. Materialy XIX mezhdunar. nauch. konf. “Reshetnevskie chteniya” posv. 55-letyu Sib. Gos. Aerokosm. Univers. ch. 1 pod red. Loginova Yu. Yu. [Materials of the XIXth Intern. Scientific Conf. “Reshetnev readings” devoted to the 55th anniversary of SibGAU named after M. F. Reshetnev]. Ch. 1. Krasnoyarsk, November 10–14, 2015, P. 153–156 (In Russ.).

10. Produktsiya OKB “Fakel”. Dvigatel K50-10.1 [The production of the experimental design bureau “Fakel”. Thruster K50-10]. Available at: http://www.fakel-russia.com/k50-10.html (accessed 18.12.2017).

11. Yermoshkin Yu. M., Raevsky V. A, Urusov V. M. [Geostationary spacecraft attitude and orbit control by motionless orbit control thrusters]. Vestnik SibGAU. 2009, No. 4 (25), P. 100–105 (In Russ.).

12. Yermoshkin Yu. M., Raevsky V. A, Urusov V. M. [Orientation and correction of the orbit of geostationary spacecraft: the scheme with the installation of correction thrusters on drives]. Vestnik SibGAU. 2010, No. 4 (30), P. 102–105 (In Russ.).

13. Ganzburg M. F., Kropotin S. A., Murashko V. M. et al. [The results of ten-year operation of electric thrusters within two telecommunication spacecraft Yamal-200 in the geostationary orbit]. Space engineering and technology. 2015, No. 4(11), P. 25–39 (In Russ.).

14. Ostrovsky V. G., Sukhov Yu. I. [Development and operation of electric thrusters and electric propulsion systems at the experimental design bureau-1 – TsKBEM – NPO “Energia” – RSC “Energia” named after S. P. Korolev (1958–2011)]. Raketno-kosmicheskaya tekhnika. Trudy. 2011. Ser. XII., Iss. 3–4, P. 122–127 (In Russ.).


Yermoshkin Yury Mikhaylovich – Cand. Sc., Docent, head of Propulsion department, JSC “Academician M. F. Reshetnev “Information Satellite Systems”. E-mail: erm@iss-reshetnev.ru.

Volkov Dmitry Viktorovich – head of Propulsion sector, JSC “Academician M. F. Reshetnev “Information Satellite Systems”. E-mail: dmitri@iss-reshetnev.ru.

Yakimov Evgeny Nikolaevich – head of Attitude control and propulsion division, JSC “Academician M. F. Reshetnev “Information Satellite Systems”. E-mail: Yen@iss-reshetnev.ru.


  ON THE CONCEPT OF ALL ELECTRIC PROPULSION SPACECRAFT