Simulation of integrated performance of aerospace plane/air-breathing propulsion system

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.