Calculation and Comparison of Liquid Oxygen Filling System between the KSLV-I Flight Test Data and the Modeling of the KSLV-II Launch Complex |
Seo, Mansu
(Launch Complex Development Team, KSLV-II R&D Head Office, Korea Aerospace Research Institute)
Lee, Jae Jun (Advanced Technology Institute, Hyundai Heavy Industries) Hong, Ilgu (Advanced Technology Institute, Hyundai Heavy Industries) Kang, Sunil (Launch Complex Development Team, KSLV-II R&D Head Office, Korea Aerospace Research Institute) |
1 | Flowmaster V7, "Flowmaster Help," Mentor Graphics Corporation, Wilsonville, O.R., U.S.A., 2015. |
2 | Lee, J.J., Park, S., Kang, S., Oh, H. 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, pp. 485-491, Nov. 2015. |
3 | Seo, M., Lee, J.J. and Kang, S., "1-D Calculation of Simultaneous Filling Operation for Three Stages of Liquid Oxygen Filling System in Korea Space Launch Vehicle-II Launch Complex," Korean Society of Propulsion Engineers Fall Conference, Jeongsun, Korea, pp. 837-845, Dec. 2016. |
4 | Park, S.Y., Kim, J.H., Park, P.G. and Yu, B.Y., "Analysis on the Filling Mode of Liquid Oxygen to the Launch Vehicle Using Flowmaster." Korean Society of Propulsion Engineers Fall Conference, Gyeong-ju, Korea, pp. 335-338, Nov. 2009. |