NSSC OpenIR  > 空间环境部
Alternative TitleThe design of Langmuir probe onboard sounding rocket
关燚炳; 王世金; 梁金宝; 刘超; 徐颖; 张爱兵; guanhuo@163.com
Source Publication地球物理学报
Keyword朗缪尔探针 空间等离子体 电离层 探空火箭
Other AbstractThe Langmuir probe,as a payload of the sounding rocket,has been designed for in situ measurements of the parameters of the ionospheric plasma in low latitude area of China and to research the fine structure of the ionosphere.The fundamental principle of the Langmuir probe has been reviewed simply.And the design of the sensor,the double probe form,the work mode of Langmuir probe and the design of the electronics has been specified.There are two identical sensors for the Langmuir probe,each with an independent preamplifier which works at the same time.A calibration test has been designed and done for the electronics of the Langmuir probe,which shows very good linearity between the input and output for the circuits.Another test for the Langmuir probe including the sensors has been done in the plasma chamber in INAF-IFSI,the first results of which indicate good performance of the payloads.
Indexed BySCI ; CSCD
Funding Project中国科学院空间科学与应用研究中心
Citation statistics
Cited Times:4[CSCD]   [CSCD Record]
Document Type期刊论文
Corresponding Authorguanhuo@163.com
Recommended Citation
GB/T 7714
关燚炳,王世金,梁金宝,等. 基于探空火箭的朗缪尔探针方案设计[J]. 地球物理学报,2012,55(6):1795-1803.
APA 关燚炳.,王世金.,梁金宝.,刘超.,徐颖.,...&guanhuo@163.com.(2012).基于探空火箭的朗缪尔探针方案设计.地球物理学报,55(6),1795-1803.
MLA 关燚炳,et al."基于探空火箭的朗缪尔探针方案设计".地球物理学报 55.6(2012):1795-1803.
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