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
|dc.identifier.citation||AIAA 2006-5195, 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 9-12 July , Sacramento, CA, 2006||en|
|dc.description.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.||en|
|dc.description.sponsorship||This paper is the part of research results which is performed in NRL Project, "The development of liquid rocket
engine with regenerative cooling system". We appreciate the related person who supports this project.
|dc.publisher||American Institute of Aeronautics and Astronautics||en|
|dc.title||A Study on Heat Transfer Characteristics of Small Liquid Rocket Engine with Calorimeter||en|
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- College of Engineering/Engineering Practice School (공과대학/대학원)Dept. of Mechanical Aerospace Engineering (기계항공공학부)Others_기계항공공학부
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