关键词: 涡轮喷气发动机;导弹推进;动态特性;计算机仿真

Abstract: The dynamic equations for regulator system and major components of turbojet engine were established by the method of variable specific heat and the model of volume accumulation. Dynamic simulation was conducted on the transient state of a turbojet engine for missile.The results show that the rotational velocity characteristics of the engine is typical,the acceleration property of the engine is good,the simulation model and the program are reliable.The key problem of the simulation and the dynamic characteristics of turbojet engine were analyzed

Key words: Turbojet engine;Missile propulsion;Dynamic characteristic;Computerized simulation