COMMUNICATION PAYLOAD INTERFACE DESIGN OF GEO SATELLITE

정지궤도위성 통신탑재체 접속설계

This paper defines the electrical interfaces and limited items to integrate Ka-band communication payload on the satellite system, which includes the detailed interfaces such as bus voltage and data bus according to the related COMS requirements. And the BUS Electrical Interface Simulator introduces to use during the course of validating and accepting between the KA-Band payload and their EGSE. These interface design results are fully validated through the testing with the BEIS and is compliant with the satellite interface control interface requirements.