발사체 자세제어를 위한 100, 250 N 급 상용 과산화수소 단일추진제 추력기 개발Development of 100, 250 N Commercial H2O2 Monopropellant Thruster for Space Launch Vehicles

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Publisher
한국추진공학회
Issue Date
2009-11-19
Language
KOR
Citation

한국추진공학회 추계학술대회

URI
http://hdl.handle.net/10203/17339
Appears in Collection
AE-Conference Papers(학술회의논문)

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