A Study on Design and Combustion Characteristic of a $H_2O_2$ /Kerosene Uni-Injector Rocket Engine
(과산화수소/케로신 단일 인젝터 설계 및 혼합비에 따른 연소특성)
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- Proceedings of the Korean Society of Propulsion Engineers Conference
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- 2010.05a
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- pp.81-84
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- 2010