概述用液体燃料冲压发动机推进的超音速导弹,可以满足某些导弹作战要求,比如射程远,高机动弹道。因此,这种发动机不同于冲压火箭发动机和超音速涡轮喷气发动机,用它后导弹的作战高度和速度可有较大变化。通过研究专门技术,得到了这种发动机的高效率:液体燃料煤油,高密度液体燃料,悬浮燃料,等等。供油系统用涡轮泵系统增压的优缺点,油箱设计。 Summary Supersonic missiles propelled by liquid fuel stamped engines meet certain operational requirements for missiles, such as long-range, high-mobility trajectories. Therefore, this engine is different from the ramjet engine and supersonic turbojet engine, use it after the missile’s combat altitude and speed can have a greater change. By researching expertise, the high efficiency of such engines is obtained: liquid fuel kerosene, high density liquid fuel, suspended fuel, and the like. Advantages and Disadvantages of Turbine Pump System Turbine System for Fuel Supply System, Tank Design.