RESEARCH PAPERS
Klink, P. and Ogawa, H., "Investigation on the performance and feasibility of RBCC-based access- to-space via multi-objective design optimization," Acta Astronautica, Vol. 157, pp. 435-454, 2019.
10.1016/j.actaastro.2018.12.034Kim, H.S., Oh, S. and Choi, J.Y., "Quasi-1D analysis and performance estimation of a sub-scale RBCC engine with chemical equilibrium," Aerospace Science and Technology, Vol. 69, pp. 39-47, 2017.
10.1016/j.ast.2017.06.019Kang, S.H. and Lee, S.Y., "Weight Reduction of the Reusable Launch Vehicles Using RBCC Engines," Journal of Korean Society of Propulsion Engineers, Vol. 17, No. 3, pp. 56-66, 2013.
10.6108/KSPE.2013.17.3.056Dong, Z., Sun, M., Wang, Z., Chen, J. and Cai, Z., "Survey on key techniques of rocket-based combined- cycle engine in ejector mode," Acta Astronautica, Vol. 164, pp. 51-68, 2019.
10.1016/j.actaastro.2019.07.016Zhao, G., Tian, Z., Pan, H., Shi, L. and He, G., "Combustion mode and heat release characteristics of a kerosene-fueled rocket-aided ramjet combustor in ramjet-to-scramjet mode transition," Aerospace Science and Technology, Vol. 141, pp. 1-12, 2023.
10.1016/j.ast.2023.108529Hiraiwa, T., Ito, K., Sato, S., Ueda, S., Tani, K., Tomioka, S. and Kanda, T., "Recent progress in scramjet/combined cycle engines at JAXA, Kakuda space center," Acta Astronautica, Vol. 63, No. 5-6, pp. 565-574, 2008.
10.1016/j.actaastro.2008.04.011Xue, R., Hu, C.B., Lv, X. and Qing, F., "RBCC constant dynamic pressure booster trajectory design and propellant mass flowrate analysis for TSTO transportation system," Journal of Solid Rocket Technology, Vol. 36, No. 2, pp. 155-160, 2013.
Shi, L., Zhao, G., Yang, Y., Gao, D., Qin, F., Wei, X. and He, G., "Research progress on ejector mode of rocket-based combined-cycle engines," Progress in Aerospace Sciences, Vol. 107, pp. 30-62, 2019.
10.1016/j.paerosci.2019.03.003Chen, J., Li, P., An, B., Sun, M., Liang, C., Wang, T., Wang, J., Li, M., Xie, Y. and Yao, Y., "Numerical study on throttling characteristics of RBCC engines in ejector mode," Case Studies in Thermal Engineering, Vol. 55, pp. 1-14, 2024.
10.1016/j.csite.2024.104150Foster, R.W., Escher, W.J.D. and Robinson, J.W., "Studies of an extensively axisymmetric rocket based combined cycle (RBCC) engine powered SSTO vehicle," Progress in Technology, Vol. 54, pp. 119- 140, 1996.
Russell, R., Brocco, D. and Daines, R., "Modeling and validation of an ejector primary rocket for shielded afterburning fuel injection," In 35th Joint Propulsion Conference and Exhibit, pp. 1-18, 1999.
10.2514/6.1999-2241Yungster, S. and Trefny, C., "Analysis of a new rocket-based combined-cycle engine concept at low speed," In 35th Joint Propulsion Conference and Exhibit, pp. 1-13, 1999.
10.2514/6.1999-2393Daines, R. and Segal, C., "Combined rocket and airbreathing propulsion systems for space-launch applications," Journal of Propulsion and Power, Vol. 14, No. 5, pp. 605-612, 1998.
10.2514/2.5352Yan, G., Wang, Y., Fan, X. and Lu, L., "Research on characteristics of shock train within mixing layer region in mixer of RBCC," In 21st AIAA International Space Planes and Hypersonics Technologies Conference, pp. 1-10, 2017.
10.2514/6.2017-2433Gu, R., Sun, M., Cai, Z., Li, P. and Huang, Y., "Numerical modeling and experimental investigation on the rocket-ejector system with limited mixer length," Acta Astronautica, Vol. 182, pp. 13-20, 2021.
10.1016/j.actaastro.2021.01.055Shi, L., Yang, Y., Yang, X., Ran, R., Qin, F. and He, G., "Experimental and numerical study on reinforcement mechanism of embedded rocket on back pressure resistance of RBCC inlet at starting stage," Aerospace Science and Technology, Vol. 123, pp. 1-11, 2022.
10.1016/j.ast.2022.107487Jian, D., Chao, H., Fei, X., Qiuru, Z. and Linyuan, P., "Numerical study on the induced-ramp mixed and combustion characteristics of rocket-based combined cycle engine," Aerospace Science and Technology, Vol. 118, pp. 1-10, 2021.
10.1016/j.ast.2021.107068Siebenhaar, A. and Bulman, M., "The strutjet engine - The overlooked option for space launch," In 31st Joint Propulsion Conference and Exhibit, pp. 1-16, 1995.
10.2514/6.1995-3124Kanda, T., Tani, K. and Kudo, K., "Conceptual study of a rocket-ramjet combined-cycle engine for an aerospace plane," Journal of Propulsion and Power, Vol. 23, No. 2, pp. 301-309, 2007.
10.2514/1.22899- Publisher :The Korean Society of Propulsion Engineers
- Publisher(Ko) :한국추진공학회
- Journal Title :Journal of the Korean Society of Propulsion Engineers
- Journal Title(Ko) :한국추진공학회지
- Volume : 28
- No :6
- Pages :16-26
- Received Date : 2024-07-22
- Revised Date : 2024-10-18
- Accepted Date : 2024-10-25
- DOI :https://doi.org/10.6108/KSPE.2024.28.6.016