Influence of plasma jets of electric jet engines on spacecraft functional characteristics

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Abstract

The issues of compatibility of correcting electric jet engines (EJE) and large-size transformable antennas (LTA) used in high-orbit communication satellites are considered. The paper deals with the erosive and polluting effect of EJE jets interacting with knitted mesh material (grid mesh), which is used for manufacturing LTA reflectors. The erosive effect of the EJE jets on the LTA mesh is characterized by the fact that the angles of ions incidence on the surface of the threads in the mesh are in the range from 0 to 90°, i. e. such effect takes place at practically any angle of ions incidence on the mesh surface. The research includes both mathematical description of physical processes and conducting a wide series of experiments, which makes it possible to achieve the necessary reliability of the results. It has been established that the effect of plasma jets of correcting engines can lead to significant sputtering of the reflecting coating from the surface of a large-size antenna reflector. The authors obtained experimental data on the degradation of the reflection coefficient of electromagnetic radiation from the mesh, depending on the degree of plasma jet influence.

It was found that the sputtering of reflecting coating from the surface of threads does not significantly affect the reflection coefficient. The sputtering of the coating at the points of threads contact is much more significant. Strong dependence of the reflection coefficient on the type of mesh weaving was also found. The mechanism of sputtering products deposition on reflecting coatings of the thermal control system radiators was investigated. The results of calculations of the sputtering coefficient and the sputtering indicatrix of the reflecting coating applied to the mesh threads were obtained. The degradation of the functional characteristics of thermoregulatory coatings (TRC) during the deposition of thin films of gold, which is one of the possible materials for a reflecting coating, was experimentally determined. Estimates of the maximum permissible level of TRC contamination were obtained. It is shown that, subject to the relevant design rules, it is possible to use EJE and LTA together in high-orbit communication satellites.

About the authors

Andrey B. Nadiradze

Moscow aviation institute (national research university)

Author for correspondence.
Email: nadiradze@mai.ru

Dr. Sc., professo; Moscow aviation institute (national research university)

Russian Federation, 4, Volokolamskoe highway, Moscow, 125993

Roman E. Tikhomirov

JSC Academician M. F. Reshetnev “Information satellite systems”

Email: tikhroman@iss-reshetnev.ru

head of the group; JSC Academician M. F. Reshetnev “Information satellite systems”

Russian Federation, 52, Lenin St., Zheleznogorsk, Krasnoyarsk region, 662972

Igor A. Maximov

JSC Academician M. F. Reshetnev “Information satellite systems”

Email: mia@iss-reshetnetv.ru

Dr. Sc., head of the department; JSC Academician M. F. Reshetnev “Information satellite systems”

Russian Federation, 52, Lenin St., Zheleznogorsk, Krasnoyarsk region, 662972

Sergey G. Kochura

JSC Academician M. F. Reshetnev “Information satellite systems”

Email: kochura@iss-reshetnev.ru

Cand. Sc., deputy general designer; JSC Academician M. F. Reshetnev “Information satellite systems”

Russian Federation, 52, Lenin St., Zheleznogorsk, Krasnoyarsk region, 662972

Sergey V. Balashow

JSC Academician M. F. Reshetnev “Information satellite systems”

Email: balashow@iss-reshetnev.ru

head of the sector; JSC Academician M. F. Reshetnev “Information satellite systems”

Russian Federation, 52, Lenin St., Zheleznogorsk, Krasnoyarsk region, 662972

References

  1. Testoyedov N. A., Kochura S. G., Maksimov I. A. [Study of the mechanisms and levels of the impact of the space environment on the spacecraft]. Vestnik SibGAU 2016, No. 6, P. 77–90 (In Russ.).
  2. Maksimov I. A., Kochura S. G. Issledovaniye vliyaniya faktorov kosmicheskogo prostranstva i tekhnogennykh faktorov na kosmicheskiye apparaty, razrabotka metodov i sredstv zashchity [Study of the influence of space factors and man-made factors on spacecraft development of methods and means of protection]. Krasnoyarsk, 2011, 182 p.
  3. Novikov L. S., Mileev V. N. et al. [Spacecraft charging in the magnetospheric plasma]. Model kosmosa, 2007, Vol. 2, 1127 p. (In Russ.).
  4. Testoyedov N. A., Kochura S. G., Maksimov I. A. et al. [Erosion impact of plasma jets of electric propulsion engines on the network of large-size aerials of automatic spacecraft]. Naukoyemkiye tekhnologii. 2016, No. 7, P. 17 (In Russ.).
  5. Vlasova N. A., Getselev I. V., Ivanova T. A. et al. [Monitoring the level of radiation conditions on high-apogee spacecraft]. Kosmonavtika i raketostroenie. 2003, No. 1(30), 6 p. (In Russ.).
  6. Sosnovets E. N., Vlasova N. A., Ivanova T. A. et al. [Control of the level of radiation impact of cosmic radiation on geostationary spacecraft Express-A2, A3 in maximum of 23th solar activity cycle (2000–2002)]. Voprosy atomnoy nauki i tekhniki. Seriya: fizika radiatsionnogo vozdeystviya na radioelektronnuyu apparaturu. 2003, No. 1–2, P. 3–7 (In Russ.).
  7. Nadiradze A. B., Rakhmatullin R. R., Kochura S. G. et al. [Features of the experimental determination of the resistance of composite materials to the erosion effect of STP]. Vestnik SibGAU. 2012, No. 1 (41), P. 91–96 (In Russ.).
  8. Tverskaya L. V., Balashov S. V., Veden’kin N. N. et al. [Outer radiation belt of relativistic electrons in the 23rd solar cycle minimum]. Geomagnetizm i aeronomiya. 2012, Vol. 52, No. 6, P. 779–784 (In Russ.).
  9. Ivanov V. V., Maksimov I. A., Nadiradze A. B. et al. [Methodology for ensuring the durability of onboard equipment and the spacecraft as a whole under SPT plasma conditions]. Vestnik SibGAU. 2006, No. 1 (8), P. 76–81 (In Russ.).
  10. Nadiradze A. B., Maksimov I. A., Smirnov V. A. et al. [An experimental study of the contaminating effect of its own external atomosphere at the stage of orbital operation of a spacecraft]. Vestnik SibGAU, 2006, No. 1 (8), P. 91–96 (In Russ.).
  11. Smirnov V. A., Shatrov A. K., Maksimov I. A. et al. [Study of the polluting effect of its own external atmosphere and plasma of SPT on spacecraft Express-AM]. Vestnik SibGAU. 2006, No. 2 (9), P. 46–50 (In Russ.).
  12. Nadiradze A. B., Chirov A. A., Shaposhnikov V. V. et al.[Computional model of plasma penetration of electric propulsion engines into instrumental compartments of spacecraft]. Vestnik SibGAU. 2006, No. 3 (10), P. 49–52 (In Russ.).
  13. Nadiradze A. B., Chirov A. A., Shaposhnikov V. V. et al. [Evaluation of the degassing time of a leaking equipment compartment]. Vestnik SibGAU. 2007, No. 1 (14). P. 95–99 (In Russ.).
  14. Maksimov I. A., Smirnov V. A., Ivanov V. V., Nadiradze A. B. [Increasing the reliability of the leaky compartment of the spacecraft]. Vestnik SibGAU. 2007, No. 1 (14), P. 88–91 (In Russ.).
  15. Smirnov V. A., Tibil’deyeva V. V., Maksimov I. A. et al. [Study of impact of SPT jets on structural elements of large-sized antennas]. Vestnik SibGAU. 2007, No. 1 (14), 7 p. (In Russ.).
  16. Ivanov V. V., Maksimov I. A., Nadiradze A. B., Shaposhnikov V. V. [Mechanisms of the effect of the plasma of electric rocket engines on the operation of the onboard equipment of spacecraft]. Vestnik SibGAU. 2007, No. 3 (16), P. 87–91 (In Russ.).
  17. Nadiradze A. B., Shaposhnikov V. V., Maksimov I. A. et al. [Selection of a ctriterion and cosiderration of the composition of pollution films when assessing the joint polluting effect of its own external atmosphere and stationary plasma engines]. Vestnik SibGAU. 2007, No 4 (17), P. 91–94 (In Russ.).
  18. Nadiradze A. B., Shaposhnikov V. V., Smirnov V. A. et al. [Study of the erosion effect of jets of SPT on radio-reflecting set-cloth of large-sized aerials of spacecraft]. Vestnik SibGAU. 2008, No. 4 (21), P. 120–124 (In Russ.).
  19. Ivanov V. V., Maksimov I. A., Nadiradze A. B., Shaposhnikov V. V., Smirnov V. A. [Model of penetration of plasma formations formed during the operation of electric propulsion engines into non-hermetic equipment compartment of spacecraft]. Materialy mezhdunarodnoy konferentsii “Aviatsiya i kosmonavtika”. Moscow, 2006, P. 357 (In Russ.).
  20. Kim V. P., Nadiradze A. B., Popov G. A. et al. [Problems of using electric rocket engines on spacecraft]. V kn. “Model’ kosmosa”, Vol. 2 «Vozdeystviye kosmicheskoy sredy na materialy i oborudovaniye kosmicheskikh apparatov». Ed. L. S. Novikova. Moscow, Universitet Publ., 2007, P. 615–659.
  21. Balashov S. V., Blyakharskiy Ya. S., Nadiradze A. B. [Calculation of sputtering characteristics of mesh surfaces when exposed to them by plasma jets of SPT]. tezisy dokladov XXI Mezhdunarodnoy konferentsii po Vychislitel’noy mekhanike i sovremennym pricladnym programmnym systemam (VMSPPS’2019). 2019, Alushta (In Russ.).

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Copyright (c) 2020 Nadiradze A.B., Tikhomirov R.E., Maximov I.A., Kochura S.G., Balashow S.V.

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