Acknowledgement
본 연구는 2021년도 정부(산업통상자원부)의 재원으로 한국에너지기술평가원의 지원을 받아 수행한 연구임(연구 번호: 20213030030100, 최대이륙중량 200kg급 비행체용 순정격출력 30 kW급 연료전지 파워팩 시스템 개발).
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