¢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