SHERP

A Study on Heat Transfer Characteristics of Small Liquid Rocket Engine with Calorimeter

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Authors
Namkoung, Hyuck-Joon; Han, Poong-Gyoo; Kim, Hwa-Jung; Lee, Kyoung-Hun; Kim, Young-Soo; Kim, Chongam
Issue Date
2006-07
Publisher
American Institute of Aeronautics and Astronautics
Citation
AIAA 2006-5195, 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 9-12 July , Sacramento, CA, 2006
Abstract
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.
Language
English
URI
http://hdl.handle.net/10371/6425
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College of Engineering/Engineering Practice School (공과대학/대학원)Dept. of Mechanical Aerospace Engineering (기계항공공학부)Others_기계항공공학부
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