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http://dx.doi.org/10.6108/KSPE.2017.21.2.102

Critical Design Result of Liquid Oxygen Filling System for Korea Space Launch Vehicle-II Launch Complex  

Seo, Mansu (Launcher Complex Development Team, KSLV-II R&D Head Office, Korea Aerospace Research Institute)
Ko, Min-Ho (Engineering Division, Aerospace Team Korea, Hanyang Engineering Co.,Ltd.)
Sun, Jeong-Woon (Engineering Division, Aerospace Team Korea, Hanyang Engineering Co.,Ltd.)
Suh, Hyun-Min (Engineering Division, Aerospace Team Korea, Hanyang Engineering Co.,Ltd.)
Lee, Jae Jun (Chemical Process Research Department, Advanced Technology Institute, Hyundai Heavy Industries)
Kang, Sunil (Launcher Complex Development Team, KSLV-II R&D Head Office, Korea Aerospace Research Institute)
Publication Information
Journal of the Korean Society of Propulsion Engineers / v.21, no.2, 2017 , pp. 102-110 More about this Journal
Abstract
In this paper, the liquid oxygen filling system (LOXFS) of the launch complex system of Korea Space Launch Vehicle-II (KSLV-II) is introduced based on critical design result by KARI in 2015 to 2016. The function and specification of the main systems of the liquid oxygen filling system, such as the storage tank, the drainage tank, the supply pumping system, the curved heat exchanger with liquid nitrogen, end valve block system, and umbilical connection, are presented.
Keywords
Liquid Oxygen Filling System(LOXFS); Launch Complex System; Korea Space Launch Vehicle-II(KSLV-II);
Citations & Related Records
Times Cited By KSCI : 1  (Citation Analysis)
연도 인용수 순위
1 Kang, S.I., Oh, H.Y. and Kim, D.R., "Basic Design of Propellant Ground Support Equipment and Flame Deflector for KSLV-II Launch Complex," Journal of the Korean Society of Propulsion Engineers, Vol. 19, No. 1, pp. 76-86, 2015.   DOI
2 Hyundai Heavy Industry CO., "KSLV-II Launch Complex Critical Design Final Report," KARI, 2016.
3 Hyundai Heavy Industry CO., HANYANG ENG CO., "Technical Description for Liquid Oxygen Filling System-K108," KARI K108.00-S-209-001-TD, 2016.
4 Hyundai Heavy Industry CO., HANYANG ENG CO., "Process Flow Diagram for LOX Filling System," KARI K108.00-S-201-001, 2016.
5 Yu, B.I., Park, S.Y., Park, P.G. and Kim, J.H., "Temperature Control System of Cryogenic Propellant for Launch Complex," Korean Society of Propulsion Engineers Fall Conference, Busan, Korea, Nov. 2011.
6 Jung, Y.S., "KSLV-II Umbilical Propellant Line Condition A.1," KARI L2-CD-00033, 2016.
7 Park, S.Y., Kim, J.H., Park, P.G. and Yu, B.I., "Analysis on the Filling Mode of Liquid Oxygen to the Launch Vehicle Using Flowmaster," Korean Society of Propulsion Engineers Fall Conference, Daejeon, Korea, Nov. 2009.
8 Lee, J.J., Park, S.M., Kang, S.I., Oh, H.Y. and Jung, E.S., "Analysis on the Filling Mode of Propellant Supply System for the Korea Space Launch Vehicle," Korean Society of Propulsion Engineers Fall Conference, Gyeong-ju, Korea, Nov. 2015.