Launch Vehicle Telemetry MUX Test by using the Spacecraft Simulator

  • Won, Young-Jin (Department of KOMPSAT-5 Systems Engineering and Integration, Korea Aerospace Research Institute) ;
  • Lee, Jin-Ho (Department of KOMPSAT-5 Systems Engineering and Integration, Korea Aerospace Research Institute) ;
  • Yun, Seok-Teak (Department of KOMPSAT-5 Systems Engineering and Integration, Korea Aerospace Research Institute) ;
  • Kim, Jin-Hee (Department of KOMPSAT-5 Systems Engineering and Integration, Korea Aerospace Research Institute) ;
  • Lee, Sang-Ryool (Satellite Research and Development Head Office, Korea Aerospace Research Institute)
  • Published : 2009.10.15

Abstract

The SAR (Synthetic Aperture Radar) satellite has the advantage of implementing the imaging mission even though it is night time, cloudy weather, and all weather conditions, which is different from the satellite with the optical payload. This is the reason why the SAR satellite comes into the spotlight in the observation satellite field. The Korea Aerospace Research Institute (KARI) has been developing the first Korean SAR satellite and is currently integrating and testing the Flight Model. For the launch vehicle service, KARI finalized the selection of the launch vehicle service provider and finished Critical Design Review (CDR) of the interface between the bus and the launch vehicle. KARI and launch vehicle service provider also finished the test of the telemetry interface between the bus and the launch vehicle. The test of the telemetry interface has the purpose of checking the interface of the telemetry which is the SOH(State-of-Health) of the satellite in an early launch stage. For this test, KARI has finished the development of the spacecraft simulator which is composed of the bus simulator to generate the analog telemetry and the launch vehicle simulator to gather the telemetry. In this research, the result of the hardware implementation and the software implementation for the spacecraft simulator were described. Finally the results of the launch vehicle telemetry MUX test which were performed at the launch vehicle provider's design office by using the spacecraft simulator were summarized. It is expected that this simulator will be used in the next test after the manufacture of the launch vehicle.

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