S-Space College of Engineering/Engineering Practice School (공과대학/대학원) Dept. of Mechanical Aerospace Engineering (기계항공공학부) Others_기계항공공학부
A Study on Heat Transfer Characteristics of Small Liquid Rocket Engine with Calorimeter
- Issue Date
- 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 9 - 12 July 2006, Sacramento, California
- Small liquid rocket engine (SLRE) with calorimeter were developed and tested to evaluate
cooling characteristics in the liquid rocket engine. Therefore, cooling performance analysis was performed to
predict the heat transfer coefficient on gas side wall in 10 calorimeter channel. A heat transfer empirical
formula was determined by results of firing test and computational simulation.
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