발사체 자세제어를 위한 100, 250 N 급 상용 과산화수소 단일추진제 추력기 개발Development of 100, 250 N Commercial H2O2 Monopropellant Thruster for Space Launch Vehicles
- Publisher
- 한국추진공학회
- Issue Date
- 2009-11-19
- Language
- KOR
- Citation
한국추진공학회 추계학술대회
- Appears in Collection
- AE-Conference Papers(학술회의논문)
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