In this study, the initial operation characteristics of a multi-type cooling system with three indoor units using an inverter compressor were investigated experimentally using a calorimeter. The operating characteristics of the cooling system were confirmed under the full load condition of simultaneous operation of three rooms and the partial load condition of individual operation of two or one room under the standard cooling conditions. The capacities of A, B and C are 50, 20, and 30% of the total capacity, respectively. The 3 room combination has 100% capacity, the 2 room combination has 50, 70 and 80% capacity, and the 1 room has 20, 30, and 50% capacity. The compressor condensing and evaporating pressures, the electronic expansion valve openings of indoor units A, B, and C, and the compressor operating frequencies were measured for 10 minutes after the cooling system was started. During the initial operation, the changes in the operating time and opening of the electronic expansion valve varied depending on the indoor unit combination and the operating load, and the relationship between the compressor pressure and the operating frequency was found.

본 논문은 공학적방벽시스템의 THM 복합거동을 분석하기 위해 구축한 In-DEBS를 실제 운영하며 취득한 운영 초기 100일간의 현장데이터에 대해 살펴보고자 한다. 콘크리트로 플러깅을 한 In-DEBS 상부에서는 콘크리트가 양생하는 동안 열을 발생하게 되어 In-DEBS의 완충재 및 근계암반에 영향을 미치게 된다. 콘크리트 플러깅에서 멀어질수록 완충재 및 근계암반의 온도는 점점 감소하게 되는데, 이러한 현상을 이용하여 센서 및 계측 시스템을 검증하였다. 처분용기를 모사한 히터는 온도제어를 통해 용기 표면 온도를 100℃로 유지할 수 있도록 설정하였으며, 시스템의 안전을 위해 일주일 동안 서서히 목표온도까지 올렸다. 히터 가동 직후 완충재의 온도는 약 4일 만에 정상상태에 도달하였으며, 상대습도는 증가하였다가 일정시간이 지난 뒤에 서서히 감소하는 것을 관찰할 수 있었다. 또한 지하수 포화에 따른 팽윤에 의해 완충재의 압력이 증가하는 것을 볼 수 있었다. 근계암반에서는 히터 가동 후 온도가 계속 증가하며, 암반의 변위도 계속 증가하는 것을 관찰할 수 있었다.

This paper describes the initial operations and preliminary results of the Instrument for the study of Stable/Storm-time Space (ISSS) onboard the microsatellite Next Generation Small Satellite-1 (NEXTSat-1), which was launched on December 4, 2018 into a sun-synchronous orbit at an altitude of 575 km with an orbital inclination angle of 97.7°. The spacecraft and the instruments have been working normally, and the results from the observations are in agreement with those from other satellites. Nevertheless, improvement in both the spacecraft/instrument operation and the analysis is suggested to produce more fruitful scientific results from the satellite operations. It is expected that the ISSS observations will become the main mission of the NEXTSat-1 at the end of 2020, when the technological experiments and astronomical observations terminate after two years of operation.