中国新一代中型运载火箭地面测发控系统架构及发展方向  

The Architecture of Test and Launch Control System in Chinese New Generation Launch Vehicle and Development Directions

作　　者：王子瑜 范瑞祥[2] 程堂明[2] 马忠辉 徐利杰 Wang Zi-yu;Fan Rui-xiang;Cheng Tang-ming;Ma Zhong-hui;Xu Li-jie(Beijing Institute of Astronautical Systems Engineering,Beijing,100076;China Academy of Launch Vehicle Technology,Beijing,100076)

机构地区：[1]北京宇航系统工程研究所,北京100076 [2]中国运载火箭技术研究院,北京100076

出　　处：《导弹与航天运载技术》2022年第2期91-97,共7页Missiles and Space Vehicles

摘　　要：运载火箭地面测发控系统主要负责实现火箭地面测试发射过程中的供配电、系统测试、参数测量、发射前控制以及故障诊断等功能,是运载火箭的重要组成部分。梳理总结了国外运载火箭地面测发控技术架构特点和发展趋势,回顾了中国长征系列火箭地面测发控技术的发展,在此基础上对新一代中型运载火箭地面测发控系统整体架构进行了详细论述。结合电气电子技术发展和未来运载火箭对地面测发控需求,提出了后续运载火箭地面测发控架构设计的发展方向和建议。Test and launch control system is one of the most important subsystems of the launch vehicle,which is responsible for power supply,system test,parameter measurement,launch control and failure diagnosis.The development trends of test and launch control system architecture of national and Long March launch vehicle in recent years are introduced.Then the test&launch system architecture in Chinese new generation launch vehicle is focused.According to the demands and features of the next generation launch vehicle,the main key technologies are put forward,which can be used as reference for the development of the future Chinese launch vehicle.

关 键 词：CZ-7/CZ-7A 运载火箭 测发控系统 架构 

分 类 号：V556[航空宇航科学与技术—人机与环境工程]