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GaInP/GaAs/Ge Triple Junction Solar Array Power Performance Evaluation on Geostationary Orbit

GaInP/GaAs/Ge 3중 접합 태양전지 배열기의 정지궤도에서 전력 성능 평가

  • Received : 2014.05.09
  • Accepted : 2014.11.13
  • Published : 2014.12.01

Abstract

The satellite on geostationary orbit accommodates multiple payloads into a single spacecraft platform and launched in June 26, 2010. The electrical power required to the satellite during sunlight is generated by a solar array wing. The solar cells are the GaInP/GaAs/Ge Triple Junction cells named Gaget2 cells from RWE Space, which were based on a Spectrolab epitaxy. This paper evaluates solar array power performance at end of design life based on the trend analysis results for the flight data on geostationary orbit. The estimated solar array power performance at end of design life compares with the power performance provided by solar array manufacturer. The solar cells show nominal behavior without significant degradation through the trend analysis results.

정지궤도위성은 다수의 탑재체를 하나의 위성체 플랫폼에 탑재하고 2010년 6월 26일에 발사되었다. 태양기간 동안 인공위성에서 요구되는 전력은 태양전지 배열기 윙에서 생성된다. 태양전지는 Spectrolab사의 적층법을 사용한 RWE Space사의 Gaget 2로 명명되는 GaInP/GaAs/Ge 3중 접합 셀이다. 본 논문은 정지궤도 비행 데이터에 대한 경향을 분석한 결과를 바탕으로 설계수명 말기에서 태양전지 배열기의 전력 성능을 평가하였다. 설계수명 말기에서 예측한 태양전지 배열기의 전력 성능은 태양전지 배열기 제작사가 제공한 전력 성능과 비교하였다. 경향분석 결과를 통해 태양전지 셀은 현저한 성능감소 없이 정상적으로 동작되고 있다.

Keywords

References

  1. H.D. Kim and all, "Remote Sensing - Advanced Techniques and Platforms - Chapter 11 COMS, the New Eyes in the Sky for Geostationary Remote Sensing," INTECH, pp. 236-268, Jun. 13, 2012.
  2. J.C. Koo, E.C. Kim, S.K. Lee and S.W. Ra, "Electrical Power Subsystem Operation in Launch and Transfer Orbits of the Geostationary Satellite," Procedding of the 2010 KSAS Fall Conference, pp. 964-967, 2010.
  3. J.C. Koo, S.K. Lee and S.W. Ra, "Solar Array Design for Geostationary Satellite," Procedding of the 2009 KSAS Spring Conference, pp. 791-964, 2009.
  4. J.C. Koo and E.C. Kim, "COMS Electrical Power Subsystem Preliminary Design," Journal of the Korea Society of Space Technology, Vol. 1, No. 2, pp. 95-100, Dec. 2006.
  5. M.D. Griffin and J.R. French, "Space Vehicle Design," American Institute of Aeronautics and Astronautics Inc., Ed. 2, pp. 490-495, 2004, Virginia, USA.
  6. A. Ketsdever, "Electrical Power Subsystem," MAE 5595, Lesson 11, University of Colorado at Colorado Springs.
  7. P. Fortescue, J. Stark and G. Swinerd, "Spacecraft Systems Engineering," John Wiley and Sons, Ed. 3, pp. 20-36, 2003, UK.
  8. R.E. Smith and G.S. West, "Space and Planetary Environment Criteria Guidelines for Use in Space Vehicle Development, 1982 Revision (Volume 1)," NASA TM-82478, pp. 1-11 to 1-12, Jan. 1983, USA.
  9. B.E. Anspaugh, "Ga/As Solar Cell Radiation Hadbook," JPL Publication 96-9, pp. 5-21 to 5-23, Jul. 01, 1996.
  10. A. Caon, C. Signorini, A. Bals and K. Dettlaff, "Multi-Junction GaAs Photovoltaic Assembly Technology for Very Severe LEO Environment Missions," 18th Space Photovoltaic Research and Technology Conference, Sep. 16-18, 2003, Ohio Aerospace Institute, USA.
  11. G. Strobl and all, "Development and Qualification Status of European Triple Junction Solar Cell for Space Applications," Proceedings of the 19th European Photovoltaic Energy Conference, Jun. 7-11, 2004, Paris, France.
  12. G.F.X. Strobl and all, "Evolution of Fully European Triple GaAs Solar Cell," Proceedings of the 7th European Space Power Conference, May 9-13, 2005, Stresa, Italy.
  13. Cell Type: 3G-27% Datasheet, Azur Space, http://www.azurspace.com.
  14. K. Dettlaff and all, "Qualification of European Triple- Junction Solar Cells with Astrium PVA Technology," Proceedings of the 8th European Space Power Conference, Sep. 14-19, 2008, Constance, Germany.
  15. J.C. Koo and S.W. Ra, "Electrical Power Subsystem Performance Evaluation of the GEO Satellite," Journal of the Korea Industrial Information System Research, Vol. 19, No. 1, pp. 31-41, Feb. 2014. https://doi.org/10.9723/jksiis.2014.19.1.031
  16. "Update on COMS Program," Report of the 38th Meeting of the Coordination Group for Meteorological Satellites, CGMS-38 KMA-WP-02, Nov. 08-12, 2010, New Delhi, India.
  17. JANS 1N5417 Datasheet, Microsemi Corp., http://www.microsemi.com.
  18. S. Cote, "Linear Analogue Sun Sensor Specification," EUR3-SP-06988-T-MMS, Astrium, Mar. 24, 2005.
  19. J.H. Park and Y.K. Chang, "Study on Power Analysis and Test Verification for STSAT-2 Solar Array," Journal of the Korea Society for Aeronautical and Space Sciences, Vol. 38, No. 5, pp. 507-517, May 2010. https://doi.org/10.5139/JKSAS.2010.38.5.507