과제정보
본 연구는 방위사업청 국방과학연구소 기초연구사업(2016-05-044)과 한국항공우주연구원이 지원하는 한국형발사체개발사업(2019M1A3A1A020-9859913)의 지원에 의해 수행되었습니다.
참고문헌
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- Lee, G.M. and Sung, H.G., "Threedimensional Effects of an Axi-symmetric Pintle Nozzle," Journal of the Korean Society of Propulsion Engineers, Vol. 22, No. 6, pp. 47-55, 2018. https://doi.org/10.6108/KSPE.2018.22.6.047
- Jeong, G.Y, Hong, J.S., Heo, J.Y., Sung, H.G., Yang, J.S. and Ha, D.S., "Thrust Characteristics of Through-type Pintle Nozzle at Operating Altitudes Conditions," Journal of the Korean Society of Propulsion Engineers, Vol. 20, No. 4, pp. 59-67, 2016. https://doi.org/10.6108/KSPE.2016.20.4.059
- Lee, G.B., Kim, J.C. and Sung, H.G., "The Analysis of Two-phase Flow in a Lean Direct Injection Gas-turbine Combustor," Journal of The Korean Society for Aeronautical and Space Sciences, Vol. 47, No. 3, pp. 204-211, 2019. https://doi.org/10.5139/JKSAS.2019.47.3.204
- Muss, A.J., Johnson, W.C., Kruse, W. and Cohn, K.R., "The Performance of Hydrocarbon Fuels with H2O2 in a Uni-element Combustor, "39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Las Vegas, N.V., U.S.A., AIAA 2003-4623, July. 2003.
- Han, D.H., Sung, H.G., Jang, S.G. and Ryu, B.T., "Parametric Analysis and Design Optimization of a Pyrotechnically Actuated Device," International Journal of Aeronautical & Space Science, Vol. 17, No. 3, pp. 409-422, 2016. https://doi.org/10.5139/IJASS.2016.17.3.409