• Proceedings of the Korea Electromagnetic Engineering Society Conference
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• 2002.11a
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• pp.86-90
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• 2002

본 논문에서는 Ka-band 위성중계기에 사용되어지는 수신하향변환기(Receiver-Downconverter) 모듈의 설계 및 제작 그리고 시험 결과에 대하여 기술하였다. 개발된 수신하향변환기는 30.6~31㎓ 대역의 신호를 입력으로 받아들여 20.8~21.2㎓ 대역의 신호를 출력하는 일종의 Downconverter 이지만, 모듈의 입력단에 저잡음 증폭부가 포함된 수신기의 역할도 하고 있다. 개발된 모듈은 제작과정 및 시험과정에 있어 위성중계기 부품 제작 규정을 준수하였으며, 그 개발된 성능은 현재까지 알려진 국내외 유사 부품중의 최고의 성능을 보여주고 있다. 측정된 모듈의 성능은 상온에서 1.9㏈의 잡음지수, 55㏈ 이득, 58dBc의 C/l3 값을 보여주고 있다. 제작된 모듈의 크기는 93mm$\times$84mm$\times$26mm이며 무게는 240g으로서 국내외 유사 제품에 비해 소형이다.

• Journal of the Korea Institute of Information and Communication Engineering
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• v.10 no.1
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• pp.184-190
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• 2006

Using COMS which provides multi-beam switching function, the optimal transmission channel environments which provides the high data rate communication are proposed in this paper. Also the link budget for communication transponder of COMSAT is designed. Bsaed on the channel modeling for group delay, non-linear and gain flatness characteristics, the system performances which provide high data rate (HDR) service were analyzed in Ka-band satellite channel. As the transmission data rate is increased, the degradation due to these channel characteristics is severely affect the system performance. To efficiently provide the various service via the same transmission system it is necessary to equlize the primary impairment factors. The optimum operating points of HDR satellite transmission system are implemeted and operated by considering the analyzed results on channel characteristics.

• The Journal of the Korea institute of electronic communication sciences
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• v.11 no.12
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• pp.1159-1164
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• 2016

This study describes the design and implementation of SHF band Low Noise Amplifier of Digital Satellite Communication. We have applied to HEMT part to minimize Noise Figure of system. and minimized the potential for the occurrence of such erroneous operation of equipment through the simulations of the space environment. We designed a reliable Low Noise Amplifier through simulation for a TID according to the vibration generated during the launch and space radiation environment, and compared pre-simulation of main performance results to test results about main performances of Low Noise Amplifier after production.

• The Journal of the Korea institute of electronic communication sciences
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• v.12 no.4
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• pp.545-548
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• 2017

This study describes the design and implementation of IFA(Input Filter Assembly) for Digital Satellite Communication. The IFA unit for SHF band consists of coupler, LPF(Low Pass Filter) and input Filter. Through the pre-simulation analysis of space environment, the possibility of the malfunction of equipment minimized and we designed a reliable IFA through simulation for vibration analysis generated during the launch, and compared pre-simulation of main performance results to test results about main performances of IFA after production.

• The Journal of the Korea institute of electronic communication sciences
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• v.12 no.6
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• pp.983-988
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• 2017

This study describes the design and implementation of OMUX(Output Multiplexer) for Satellite Communication. The OMUX unit for SHF band consists of LPF(Low Pass Filter), manifolder and Channel Filter. Through the pre-simulation analysis of space environment, the possibility of the malfunction of equipment minimized and we designed a reliable OMUX through simulation for vibration analysis generated during the launch, and compared pre-simulation of main performance results to test results about main performances of OMUX after production.

• Proceedings of the Korean Institute of Communication Sciences Conference
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• 1995.10a
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• pp.783-786
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• 1995

• The Magazine of the IEIE
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• v.25 no.1
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• pp.40-48
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• 1998

• Proceedings of the Korean Institute of Information and Commucation Sciences Conference
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• v.9 no.1
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• pp.1113-1116
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• 2005

Using COMSAT which provides multi-beam switching function, the optimal transmission channel environment which provides the high data rate communication are proposed in this paper. Also the link budget for communication transponder of COMSAT is designed. Based on the channel modeling for group delay, non-linear and gain flatness characteristics, the system performances which provide various data rate services were analyzed in Ka-band satellite channel. As the transmission data rate is increased, the degradation due to these channel characteristics is severely increased. The linear component of group delay and the AM-AM component of non-linear characteristics severely affect the system performance. To efficiently provide the various service via the same transmission system it is necessary to equalize the primary impairment factors. The optimum operating points of HDR satellite transmission system are implemented and operated by considering the analyzed results on channel characteristics.

• Electronics and Telecommunications Trends
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• v.21 no.4 s.100
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• pp.107-117
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• 2006

위성 탑재체 제조 산업은 기초 과학이 뒷받침된 초정밀 기계 공학, 첨단 전자 기술, 극한 환경 기술 및 신소재 공학 등과 같은 첨단 산업의 집합체라 할 수 있다. 현재 미국을 비롯한 서구 선진국에서 진행중인 탑재체 기술동향을 보면, 폭발적으로 증가하는 위성수에 따라 위성 궤도가 부족하고 주파수 자원이 고갈되고 있는 상황에서 통신 위성의 효율성과 성능을 향상시킬 수 있는 신호처리 탑재(OBP) 위성과 통신기능을 포함한 다양한 기능을 가진 복합위성 개발이 진행되고 있으며 주파수 대역의 포화와 광대역 멀티미디어 서비스 제공 등을 위해 보다 높은 주파수의 준 밀리미터파 대역(Ka 대역) 위성 개발이 활발히 이루어지고 있다. 국내에서는 현재, 2008년 발사를 목표로 마이크로스위치 매트릭스(MSM)가 탑재되어 빔간 스위칭이 가능하도록 설계된 통신해양기상위성(COMS)용 통신 탑재체(SACOM) 개발이 진행중이다. 국내의 위성탑재용 RF 부품분야는 1990년부터 위성 중계기 시스템의 기본적인 설계, 조립, 종합화, 시험기술을 바탕으로 통신위성 탑재체용 초고주파 부품을 개발하여 왔으며, 2000년대에는 Ku 대역(12/14GHz) 및 Ka 대역(20/30GHz) 기술인증모델(EQM) RF 부품을 성공적으로 개발하였다. 이를 바탕으로 통신해양기상위성 통신탑재체용 Ka 대역 RF 부품이 현재 우주인증 모델(QM)의 개발이 완료되었으며 비행 모델(FM) 개발이 진행중이다.

• The Journal of Korean Institute of Electromagnetic Engineering and Science
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• v.13 no.1
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• pp.7-11
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• 2002

A novel microstrip type law-pass filter using thin or thick film resistors is proposed to efficiently eliminate harmonic spurious response in stop-band. The proposed low-pass filter shows the spurious suppression enhancement of 20 dB over a conventional one. The designed low-pass filter could be used as a harmonic rejection filter of a local oscillator for Ku-band satellite payload system.