关键词: 航天运输系统;涡轮风扇发动机;冲压喷气发动机;进气道-发动机匹配;飞机-发动机匹配;数值仿真

Abstract: The integrated performance of aero space plane/air breathing propulsion system was simulated.Choosing method of main design parameters of turbo and ramjet were described.Based on given design parameters,the engine performance was computed along flight trajectory.An engineering method was used to compute the characteristics of induction system and exhaust system.According to the approach of force accounting,the integrated performance of vehicle/air breathing propulsion system was calculated.

Key words: Space transportation system;Turbofan engine;Ramjet engine;Inlet engine matching;Airplane engine matching;Numerical simulation