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Radio Occultation Mission in Korea Multi-Purpose Satellite KOMPSAT-5

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Abstract

The first occultation mission in the Korean space program, KOMPSAT-5, is scheduled for launch in 2010. KOMPSAT-5 will have a dual frequency GPS receiver to generate precision orbit determination data and occultation data. The KOMPSAT-5 spacecraft and the characteristics of its occultation payload are described in this paper. An occultation processing system developed by KASI is also introduced.

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References

  • Kirchengast G, Fritzer J, Ramsauer J (2002) End-to-end GNSS Occultation Performance Simulator Version 4 (EGOPS4) Software User Manual. Tech. Rep. 3, IGAM/UG Technical Report for ESA/ESTEC, Institute for Geophysics, Astrophysics, and Meteorology, Univ of Graz, Austria

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  • Lee S (2007) Introduction of KOMPSAT-5 Program. 1st AOPOD Workshop 2007, Jeju Island, Korea

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  • Lee W, Chung J, Cho S, Park J, Cho J, Yoon J, Lee J, Chun Y, Lee S (2007) Retrieval of electron density profile for KOMPSAT-5 GPS radio occultation data processing system. J Astron Space Sci 24(4):297–308

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Correspondence to S. Cho .

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© 2009 Springer-Verlag Berlin Heidelberg

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Cho, S., Chung, J., Park, J., Yoon, J., Chun, Y., Lee, S. (2009). Radio Occultation Mission in Korea Multi-Purpose Satellite KOMPSAT-5. In: Steiner, A., Pirscher, B., Foelsche, U., Kirchengast, G. (eds) New Horizons in Occultation Research. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-00321-9_22

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