| Citation: | DU Jinfeng, JIA Linyuan, CHEN Yuchun, et al. Comparative analysis on aircraft and engine integration performance of RBCC engines with different fuels[J]. Journal of Aerospace Power, 2024, 39（8）：20230310 doi: 10.13224/j.cnki.jasp.20230310
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In order to study the impact of different fuels on the overall performance of rocket based combined cycle (RBCC) engines, a quasi-one-dimensional overall performance simulation model of RBCC engines was built. The thrust and specific impulse performance of RBCC engines fueled with liquid oxygen kerosene, hydrogen peroxide kerosene, liquid oxygen methane, and liquid oxygen liquid hydrogen were studied. Combined with the integrated aircraft engine performance analysis model, the effects of different fuel engine performance on flight mission capability were studied. The results showed that at ejector mode, the thrust of hydrogen fuel was 1.3 times greater than kerosene fuel; the hydrogen fueled RBCC engine had the farthest cruising distance of 4470 km; under the same aircraft parameters, hydrogen peroxide kerosene fuel RBCC powered aircraft had the highest maneuverability. This method can provide a reference for the overall performance scheme design and fuel selection of RBCC engines.
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