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한국추진공학회지 = Journal of the Korean Society of Propulsion Engineers, v.24 no.6, 2020년, pp.45 - 52
이선영 (Rocket Propulsion, Mechanical R&D, LIG Nex1) , 이현섭 (Rocket Propulsion, Mechanical R&D, LIG Nex1) , 양희성 (Rocket Propulsion, Mechanical R&D, LIG Nex1) , 길태옥 (Rocket Propulsion, Mechanical R&D, LIG Nex1) , 김동욱 (R&D Lab, LIGPOONGSAN Protech) , 방제훈 (R&D Lab, LIGPOONGSAN Protech) , 최성호 (Ground Technology Research Institute, Agency for Defense Development) , 이용선 (Ground Technology Research Institute, Agency for Defense Development)
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In this paper, a subminiature solid rocket motor(SSRM) was designed to develop a miniature smart-bullet and the designed propellant grain was made of thermoplastic propellant for production convenience of inner shape. The internal ballistics analysis and ground test were performed to investigate the...
Lee, S.H., Cho, H.J., Cho, Y.K. and Bang, H.C., "Recent status on Miniature Smart-bullet Techniques", J. of the Korean Society for Aeronautical and Space Sciences, Vol. 34, No. 3, pp. 272-281, 2015.
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Lee, H.G., Jung, H.Y., Cho, J.H., Lee, Y.G. and Lee, H.J. "Study of the Inhibition on the Combustion of PEBAX/AP Thermoplastic Propellant", Journal of the Korean Society of Propulsion Engineers, Vol. 17, No. 5, pp. 301-309, 2019.
Trache, D., Maggi, F., Palmucci, I., DeLuca, L.T., Khimeche, K., Fassina, M., Dossi, S. and Colombo, G., "Effect of amide-based compounds on the combustion characteristics of composite solid rocket propellants" Arabian Journal of Chemistry, Vol. 12, pp. 3639-3651, 2019.
Ghorpade, V.G., Dey, A., Jawale, L.S., Kotbagi, A.M., Kumar, A., and Gupta. M., "Study of Burn Rate Suppressants in AP-Based Composite Propellants" Propellants Explos. Pyrotech., Vol. 35, No. 1, pp. 53-56, 2010.
Ryu, T.H., Jung, E.H., Lee, K.Y., Choi, J.S., Khil, T.O., Kim, M.H., Cho, J.H., Lee, Y.S. and Choi, S.H., "Optimal Design of Tiny Rocket Propulsion System Using Thermoplastic Solid Propellant" KSPE Spring Conference, pp. 301-309, May 2019.
Kang, S.I. and Huh, H.I., "A CFD Study for Rocket Exhaust Flow Using Single Species, Unreacted Flow Model," Aerospace Engineering and Technology, Vol. 11, No. 1, pp. 126-134, 2012.
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