宇航计测技术
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刘靖1;刘志强1
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作者简介:
LIU Jing1;LIU Zhi-qiang1
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摘要: 根据武器系统试验需求,提出了超音速靶机的总体技术要求。按照飞行器设计的基本流程,完成了某型超音速靶机的总体设计,对该型靶机的动力系统、气动布局、气动特性等方面进行了详细设计,并对主要飞行性能进行了计算,为超音速靶机的工程实现打下了基础。
关键词: 飞行器, 超音速靶机, 总体设计
Abstract: According to the requirements of test and evaluation of weapon system, the general technology requirements were put forward. The conceptual design of supersonic target drone on the aircraft design procedure was finished. The dynamic system, aerodynamic configuration and aerodynamic characteristics were designed in detail. The main flight performance was calculated. The foundation of engineering implementation for the supersonic target drone has laid by the conceptual design.
Key words: Aircraft, Supersonic target drone, Conceptual design
刘靖;刘志强. 超音速靶机的总体设计与研究[J]. 宇航计测技术, doi: 10.12060/j.issn.1000-7202.2016.04.12.
LIU Jing;LIU Zhi-qiang. Conceptual Design and Reserch of Supersonic Target Drone[J]. JOURNAL OF ASTRONAUTIC METROLOGY AND MEASUREMENT, doi: 10.12060/j.issn.1000-7202.2016.04.12.
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http://www.yhjcjs.com.cn/CN/Y2016/V36/I4/60