Comparative evaluation of the effectiveness of the application of perspective types of electric propulsion thrusters in the small spacecraft

Abstract


The report includes comparative analysis of efficiency in the use of small spacecraft with electric propulsion based on ion thrusters, stationary plasma thrusters and pulsed plasma thrusters.


About the authors

V. M. Kulkov

Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute (National Research University)

Author for correspondence.
Email: riame@sokol.ru

Russian Federation

Candidate of Engineering Science

Senior Researcher, Head of Department

V. A. Obukhov

Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute (National Research University)

Email: riame@sokol.ru

Russian Federation

Candidate of Engineering Science

Senior Researcher, Vice Director

Y. G. Yegorov

Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute (National Research University)

Email: riame@sokol.ru

Russian Federation

Designer

A. A. Belik

Research Institute of Applied Mechanics and Electrodynamics of Moscow Aviation Institute (National Research University)

Email: riame@sokol.ru

Russian Federation

Candidate of Engineering Science

Senior Researcher, Head of Sector

A. M. Krainov

Scientific-Production Association named after S. A. Lavochkin, Moscow

Email: ztk-tol@mail.ru

Russian Federation

Senior Specialist

References

  1. Electric Propulsion Activity in Russia [Text] / V. Kim, A. Koroteev, V. Muroshko [et al.] // 27-th IEPC. Pasadena, USA, 2001.
  2. Juergen Mueller. Thruster Options for Microspacecraft: A Review and Evaluation of State-of-the-Art and Emerging Technologies. Progress in Astronautic and Aeronautic. Vol. 187. 2000, pp. 45-137.
  3. Ким, В. Разработка и исследование малых СПД [Текст] / В. Ким [и др.] // AIAA-98-3335, Cleveland, USA. Paper AIAA-2003-5002, 39-th Joint Propulsion Conference, Huntsville (USA), 2003.
  4. Evaluation of low power Hall thruster propulsion [Text] / V.Kim, A.Semenkin [et al.] // AIAA, ASME, SAE and ASEE Joint Propulsion Conference and Exhibit, 32 nd, Lake Buena Vista, FL, July, 1-3, 1996.
  5. Интернет-сайт: www.fakel-russia.com.
  6. Laboratory Investigation of Pulsed Plasma Thrusters with Gas Valves [Text] / N. Antropov, G. Diakonov, O. Lapaev [et al.] // Micropropulsion for Small Spacecraft. Progress in Astronautic and Aeronautic. 2000. - Vol. 187. - P. 369-377.
  7. Дьяконов, Г.А. Экспериментальные исследования моделей АИПД малой мощностью [Текст] / Г.А. Дьяконов, Н.В. Любинская, С.А. Семенихин // Авиационно-космическая техника и технология. - 2009. - №9 (66). - С. 136-138.
  8. Pulsed plasma thrusters for spacecraft attitude and orbit control system / N.N. Antropov [et. al.]. Paper IEPC-99-192. - P. 1129-1135.
  9. Разработка вариантов малых космических аппаратов с электроракетными двигателями и режимов управления ими для решения задач в околоземном космическом пространстве [Текст] / Г.А. Попов, В.А. Обухов, В.М. Кульков [и др.] // IV Междунар. конф.-выставка "Малые спутники. Новые технологии. Миниатюризация. Области эффективного применения в XXI веке". - Королёв, Моск. обл, 2004.
  10. Сравнительный анализ двигательных установок для низкоорбитальной группировки малых КА [Текст] / Ю.Г. Егоров, В.М. Кульков, В.А. Ламзин [и др.] // III-я междунар. конф. по малым спутникам. – Королев, Моск. обл. - 2002.

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