Search > Reference Search
Search Result
학술지
No Reference Title /Author/Journal Title Citing Article
1 Adel, W.M., “Service life prediction of AP/Al/HTPB solid rocket propellant with consideration of softening aging behavior,” Chinese Journal of Aeronautics, Vol. 32, No. 2, pp. 361-368, 2019./   DOI View Article
2 Park, J.H., Ryu, N.S., Park, J. B. and Jung, G.D., "Natural Aging Properties Analysis of HTPB Propellant," Journal of the Korean Society of Propulsion Engineers, Vol. 23, No. 1, pp. 9-14, 2019./ View Article
3 Yu, S., Jo, S., Kim, H. J. and Kim, S-L., "A 1-D Start-up Analysis for Liquid Rocket Engine Powerpacks," Journal of the Korean Society of Combustion, Vol. 24, No. 1, pp. 39-45, 2019./   DOI View Article
4 Ko, S.H., "A Study on the Combustion Characteristics of Liquefying Solid Fuel Followed Shape of Post-Chamber for Hybrid Rocket Propulsion System," Master, Department of Aerospace and Mechanical Engineering, Korea Aerospace University, Goyangsi, Gyeonggi-ddo, Korea, 2019./ View Article
5 "Space Launch Report: SpaceX Falcon 9 v1.2 Data Sheet," World Wide Web location_ http://www.spacelaunchreport.com/falcon9ft.html, updated May 04, 2019/ View Article
6 Jetcat products manual, "Jetcat-P300-RX ", World Wide Web Location http://www.jetcat.de/en/productdetails/, 2019./ View Article
7 Hwang, K.Y. and Park, J.K., “Characteristics and Development Trends of Heat-Resistant Composites for Flight Propulsion System,” Journal of The Korean Society for Aeronautical and Space Sciences, Vol. 47, No. 9, pp. 629-641, 2019./   DOI View Article
8 Bae, J.Y., Hwang, K.Y. and Ham, H.C., "Development Report of Fluent-2C Software for Coupled Flow/Thermal Response Analysis of Rocket Nozzle," ADD Report, ADDR-421-191945, 2019./ View Article
9 Hwang, D., Bak, S., and Ahn, K., “Preliminary Combustion Tests in Bi-Swirl Coaxial Injectors Using Gaseous Methane/Gaseous Oxygen Propellants,” Journal of the Korean Society of Propulsion Engineers, Vol. 23, No. 4, pp. 70-80, 2019./   DOI View Article
10 Jang M.W., Kim T.K., Han H.J., Yun J.H. and Son H.I.,"A Study on The Property of NEPE System Propellant with Respect to The Size of RDX," Journal of the Korean Society of Propulsion Engineers, Vol. 22, No. 3, pp. 40-45, 2018./   DOI View Article