¢º Thrust Vector Control
¢º Rocket Launcher System
Evaporation of Multi- Component Droplet in High Pressure(Experimental study)
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Propulsion & Combustion Lab., Div. of Aerospace Eng., School of Mechanical, Aerospace & Systems Eng., KAIST,
373-1, Guseong-Dong, Yuseong-Gu, Daejeon, Korea Tel: +82-42-350-3754/5754, FAX: +82-42-350-3710