子午工程探空火箭伸杆展开机构技术研究

	子午工程探空火箭伸杆展开机构技术研究
	杨萱 ; 杨华 ; 孙健 ; 邹向荣 ; 马鑫 ; 周伟
刊名	空间科学学报
	2013
卷号	33 期号:6 页码:678-682
关键词	子午工程探空火箭套筒式伸杆展开机构电子伸杆电场伸杆
ISSN号	0254-6124
其他题名	Research on Meridian Project Sounding Rocket Boom Deploying Technology
通讯作者	北京8701信箱
中文摘要	根据子午工程探空火箭电子和电场探测需求,设计了套筒式伸杆展开机构.通过电子伸杆和电场伸杆的结构方案设计、力学仿真分析,伸杆单项力学试验,伸杆与整箭的匹配力学试验以及伸杆飞行试验验证得出,该伸杆技术方案合理可行,伸杆总体构型、布局设计及结构方案设计满足科学探测各项技术指标的要求。
英文摘要	Based on the needs of Meridian Project of sounding rockets' electronic and electric field probe, a sleeve-type of boom deployment mechanism was designed. Structure scheme design, mechanical simulation analysis, single mechanical property test, the whole rocket matching mechanical test as well as the flight test validation of both electronic boom and the electric field boom showed that the boom technical scheme is reasonable and feasible, and the boom overall configuration, layout design and structure design can meet the requirements of technical index for scientific exploration. According to the scientific exploration mission needs and space restrictions of the installation on the sounding rocket, a wide range of innovative design and development are carried out in the structure style, deployment and motion mode, locking and fixed mechanism of the boom deployment mechanism, as well as its installation on the rocket and release, etc.
学科主题	空间技术
语种	中文
内容类型	期刊论文
源URL	[http://ir.cssar.ac.cn/handle/122/722]
专题	国家空间科学中心_空间技术部
推荐引用方式 GB/T 7714	杨萱,杨华,孙健,等. 子午工程探空火箭伸杆展开机构技术研究[J]. 空间科学学报,2013,33(6):678-682.
APA	杨萱,杨华,孙健,邹向荣,马鑫,&周伟.(2013).子午工程探空火箭伸杆展开机构技术研究.空间科学学报,33(6),678-682.
MLA	杨萱,et al."子午工程探空火箭伸杆展开机构技术研究".空间科学学报 33.6(2013):678-682.