摘要
为检验TSPR能否用于战术飞行器并实现预定的飞行任务目标,文中以HARM导弹为研究对象,通过进行驱动HARM导弹的TSPR方案设计和弹道性能研究,得出:设计得到的TSPR呈串联布局,总质量约为180 kg,总长3.55 m;TSPR驱动的HARM导弹能够从(3 km、Ma 0.9)加速爬升至(10 km、Ma 2.2)状态巡航,总射程达到280.6 km,是同等质量固体发动机驱动射程的3.9倍,平均速度约为固体发动机驱动的1.1倍,证明了TSPR是优良的战术飞行器推进系统。
In order to test whether the TSPR-powered tactical aircraft can achieve the intended mission objectives,taking HARM missile as research object,this paper carried on the design and the trajectory of the TSPR-driven HARM missile.It is concluded that the total mass of TSPR which is series connection is about 180 kg and the total length is 3.55 m.The TSPR-driven HARM missile can accelerate from(3 km、Ma 0.9)to cruise state(10 km、Ma 2.2),with a total range of 280.6 km,which is 3.9 times the range of the same quality solid rocket motor drive,and the average speed is about 1.1 times that of the solid rocket motor.It is proved that TSPR is an excellent tactical aircraft propulsion system.
作者
陈莎
杨昀
李江
刘凯
CHEN Sha;YANG Yun;LI Jiang;LIU Kai(National Key Laboratory of Combustion Flow and Thermo-structure,Xi’an Insitute of Aerospace Propulsion Technology,Xi’an 710025,China;The Fourth Academy of CSAC,Xi’an 710025,China;National Key Laboratory of Combustion Flow and Thermo-structure,Northwestern Polytechnical University,Xi’an 710072,China)
出处
《弹箭与制导学报》
北大核心
2020年第3期55-59,共5页
Journal of Projectiles,Rockets,Missiles and Guidance
