Acknowledgement
본 연구는 서울대학교 미래혁신연구원과 연계된 2022년 정부(과학기술정보통신부)의 재원으로, 한국연구재단 스페이스챌린지사업(2021M1A3B8075809)의 지원과 한국연구재단의 지원(NRF-2021R1A2C2003759), 그리고 서울대학교 항공우주신기술연구소의 지원을 받아 수행된 결과입니다.
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