Browse > Article
http://dx.doi.org/10.6108/KSPE.2014.18.1.085

Design of Compressed Gas Supply System for Combustion Chamber Test Facility  

Chung, Yonggahp (Propulsion Test and Evaluation Team, Korea Aerospace Research Institute)
Cho, Namkyung (Propulsion Test and Evaluation Team, Korea Aerospace Research Institute)
Han, Yeoungmin (Propulsion Test and Evaluation Team, Korea Aerospace Research Institute)
Publication Information
Journal of the Korean Society of Propulsion Engineers / v.18, no.1, 2014 , pp. 85-90 More about this Journal
Abstract
To develop liquid propulsion engine, the development of combustion chamber must be preceded. For performance validation of the combustion chamber, the designed and manufactured combustion chamber should be tested in combustion chamber test facility (CCTF). The CCTF is the test facility to develop the combustor of rocket engine, which uses liquid oxygen as a oxidizer and kerosene as a fuel. Present paper introduces the detailed design results of compressed gas supply system of CCTF, which is planned to be installed at Naro Space Center.
Keywords
Combustion Chamber Test Facility(CCTF); Compressed Gas; Supply System; Hydraulic and Pneumatic; Design;
Citations & Related Records
Times Cited By KSCI : 2  (Citation Analysis)
연도 인용수 순위
1 Lee, K.J, Lim, B.J., Seo, S.H., Han, Y.M., and Choi, H.S., "Sub-System Requirements of a Pressured-fed Hot-firing Test Facility for the Performance Assessment of a LRE Thrust Chamber," Journal of the Korean Society of Propulsion Engineers, Vol. 15, No. 4, pp. 94-102, 2011.   과학기술학회마을
2 Chung, Y.G., Cho, N.K., and Han, Y.M., "Modeling and Simulation of Combustion Chamber Test Facility Oxidizer Supply System," Journal of the Korean Society of Propulsion Engineers, Vol. 16, No. 6, pp. 92-97, 2012.   과학기술학회마을   DOI   ScienceOn