The feature of raising the “Express-AMU3” and “Express-AMU7” satellites into geostationary orbit

Автор: Yu. M. Ermoshkin, A. A. Vnukov, D. V. Volkov, Yu. V. Kochev, R. S. Simanov, E. N. Yakimov, S. Yu. Pridannikov

Журнал: Siberian Aerospace Journal @vestnik-sibsau-en

Рубрика: Aviation and spacecraft engineering

Статья в выпуске: 4 vol.23, 2022 года.

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At present, in order to increase the launch mass, raising satellites into geostationary orbit by their own propulsion subsystem is widely used. Oly the JSC “Academician M. F. Reshetnev “Information Satellite Systems” applied such a scheme for several satellites of their own design - "Express-AM5", "Express-AM6", "Express-80" and "Express-103". Along with this, some diversity of approaches to the implementa-tion of this operation can be noted. In particular, the orbit raising of the above satellites was carried out using the onboard propulsion subsystem based on SPT-100 plasma thrusters. The operation was carried out by one or two thrusters. The use of two thrusters of the "Express-80" and"Express-103" satellites was due to the desire to keep within a reasonable amount of no more than six months with a significant increase in the output mass. Nevertheless, the duration of the orbit raising of about 150 days, which took place dur-ing the raising of satellite data, is also excessively long. It is evidemnt that it can be reduced, other things being equal, only by increasing the available thrust of the thrusters. This can be achieved both by increas-ing the thrust of individual units, and by increasing the number of simultaneously used thrusters. Therefore, for the new Express-AMU3 and Express-AMU7 satellites (with dimensions similar to the Express-80 and Express-103 satellites), for which a paired launch was also assumed, both of these methods were used. For orbit raising, two SPT-100V thrusters and, additionally, an SPT-140D type thruster were used. The total thrust of a cluster of thrusters made it possible to count on a significant reduction in the duration of orbit raising in comparison with the Express-80 and Express-103 satellites. The SPT-140 thruster developed by JSC "Experimental Design Bureau FAKEL" was used in Russia for the first time. For its power supply, the CCS-140D control and conversion device was specially created at the JSC "Design Bureau Polyus". The use of a combination of three thrusters made it possible to significantly reduce the duration of the opera-tion of raising into geostationary orbit.

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Plasma thruster, satellite, orbit raising, power processing unit, orbit control

Короткий адрес: https://sciup.org/148329662

IDR: 148329662   |   DOI: 10.31772/2712-8970-2022-23-4-696-707

Список литературы The feature of raising the “Express-AMU3” and “Express-AMU7” satellites into geostationary orbit

  • Ermoshkin Yu. M., Vnukov A. A., Volkov D. V. et al. [Application of the propulsion subsystem based on the SPD-100V plasma engine for the additional ascent and correction of the orbit of the Ex-press-80 and Express-103 spacecraft]. Siberian Aerospace Journal. 2021, Vol. 22, No. 3, P. 480–493 (In Russ.). Doi: 10.31772/2712-8970-2021-22-3-480-493.
  • Qualification of the SPT-140 for use on western Spacecraft / J. Delgado, R. Corey, V. Murashko, A. Koryakin, S. Pridannikov. AIAA-2014-3606, 50th Joint Propulsion Conference, Cleveland, Ohio, 2014, USA, July 28–30. 13 p.
  • Casaregola C. Electric Propulsion for Station Keeping and Electric Orbit Raising on Eutelsat Platform. Joint Conference of 30th ISTS, 34th IEPC, 6th NSAT, Kobe-Hyogo, Japan, July 4–10, 2015, IEPC-2015-97. 6 p
  • Komarov A., Pridannikov S., Lenguito G. Typical transient phenomena of Hall Effect thrusters. IEPC-2019-304. Proc. of the 36th International Electric Propulsion Conference, Vienna, Austria, 2019. 10 p.
  • Lovtsov A. S., Selivanov M. Yu., Tomilin D. A. et al. [Main results of developments by the Keldysh Center in the field of electric propulsion systems]. Izvestiya RAN. Energy. 2020, No. 2, P. 1–13 (In Russ.).
  • 30 years of Electric Propulsion Flight Experience at Aerojet Rocketdyne / W. Hoskins, R. Cas-sady, R. Myers et al. 33rd international Electric Propulsion Conference, The George Washington Uni-versity, Washington, D.C., USA, October 6-11, 2013. IEPC-2013-439. 12 p.
  • Duchemin O., Rabin J., Balika L. et al. Qualification Status of the PPS-5000 Hall Thruster Unit. 36th International Electric Propulsion Conference. University of Vienna, Austria, Sept. 15–20, 2019, 13 p. IEPC-2019-906.
  • Mullins C., Hruby V., Pote B. et al. Development of a 5kW Class Hall Thruster. 36th Interna-tional Electric Propulsion Conference, University of Vienna, Austria, Sept. 15–20, 2019. 15 p. IEPC-2019-492.
  • Hruby P., Demmons N., Courtney D. et al. Overview of Busek Electric Propulsion. 36th Inter-national Electric Propulsion Conference, University of Vienna, Austria, Sept. 15–20, 2019, 13 p. IEPC-2019-926.
  • Pyatykh I., Bernikova M., Gopanchuk V.et al. Development of stationary thruster SPT-230 with discharge power 10–15 kW. 35th International Electric Propulsion Conference, Georgia Institute of Technology, Atlanta, Georgia, USA, October 8–12, 2017. 8 p. IEPC-2017-548.
  • Lovtsov A., Tomilin D., Muravlev V. [Development of high-voltage Hall motors in the Keldysh Center]. 68th International Astronautical Congress (IAC), Adelaide, Australia, 25–29 September 2017. 5 p.
  • Jonson I., Kay E., Lee T. et al. New Avenues for research and Development of Electric Propul-sion Thrusters at SSL. 35th International Electric Propulsion Conference, Georgia Institute of Tech-nology, Atlanta, Georgia, USA, October 8–12, 2017. 16 p. IEPC-2017-400.
  • Bourguignon E., Fraselle S. PPU Mk3 for 5 kW Hall Effect Thruster. The 35th International Electric Propulsion Conference, Georgia Institute of Technology, Atlanta, Georgia, USA, October 8–12, 2017. 6 p. IEPC-2017-171.
  • Pinto F., Palencia J., Glorieux G., Wagner N. Airbus Defence and Space Power Processing Units: New HET and GIT PPU developments Qualification Status. 35th International Electric Propul-sion Conference, Georgia Institute of Technology, Atlanta, Georgia, USA, October 8–12, 2017. 8 p. IEPC-2017-266.
  • Vnukov A. A., Babanov A. A., Doronkin M. N. et al. Sposob vyvedeniya kosmicheskogo appa-rata na geostatsionarnuyu orbitu s ispol'zovaniyem dvigateley maloy tyagi [A method for launching a spacecraft into a geostationary orbit using low-thrust engines]. Patent RF, No. 16, 2016.
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