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http://dx.doi.org/10.5139/JKSAS.2006.34.2.106

Development of Combustion Test Facility for Liquid Rocket Engine  

Kim, Dong-Hwan (㈜ 로템)
Lee, Seong-Ung (㈜ 마이크로프랜드)
Yu, Byeong-Il (한국항공우주연구원)
Publication Information
Journal of the Korean Society for Aeronautical & Space Sciences / v.34, no.2, 2006 , pp. 106-111 More about this Journal
Abstract
Combustion test facility for liquid rocket engine using kerosene and liquid oxygen has been developed for the purpose of cooling and performance study. Test engine of thrust under 1.0 KN can be evaluated, and the real combustion test ensures a good operation of the combustion test facility. Combustion test facility will be modified to supply natural gas and liquefied natural gas as fuel and to give a regenerative cooling test.
Keywords
Combustion Test Facility; Propellant Cooling; Liquid Rocket Engine;
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