A rocket-based combined-cycle (RBCC) inlet is always required to start at a relatively low Mach number in consideration of the fuel consumption in the ejector mode and the comprehensive engine performance throughout the flight trajectory. However, ...

中文翻译：

---

RBCC 入口的起始限制和正控制

考虑到喷射器模式下的燃料消耗和整个飞行轨迹的综合发动机性能，基于火箭的联合循环（RBCC）进气道总是需要在相对较低的马赫数下启动。然而， ...