과제정보
본 연구는 한국항공우주연구원의 2단형 소형발사체선행기술개발사업(FR22B00)과 한국연구재단(과학기술정보통신부)의 스페이스챌린지사업(2021M1A3B807777112)의 지원을 받아 수행되었습니다.
참고문헌
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