System Requirement of Regenerative Fuel Cell for a Stratospheric Airship

성층권비행선용 재생연료전지 시스템 요구사양

  • 정용운 (한국항공우주연구원, 비행선그룹) ;
  • 이융교 (한국항공우주연구원, 비행선그룹) ;
  • 강왕구 (한국항공우주연구원, 비행선그룹) ;
  • 김동민 (한국항공우주연구원, 비행선그룹) ;
  • 염찬홍 (한국항공우주연구원, 항공체계실장)
  • Published : 2005.06.01

Abstract

The effort to realize the concept of stratospheric airship, which can fly at about 20km altitude, has been persevered since late 1980's. Referring to the feasibility study of ensuring the flight duration of the airship over 1year, total weight is about 30 tons, the length is about 200m. There are lots of key technologies to be solved to develop the system, and one of the essential prerequisite technologies is regenerative fuel cell system. In this paper, design requirement of regenerative fuel cell system is introduced with the feasibility study results of the challenging stratospheric airship.

Keywords