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The Experimental Satellite on Electromagnetism Monitoring
作者姓名:Shen  Xuhui
作者单位:Institute of Earthquake Science, China Earthquake Administration, Beijing 100036
摘    要:The Experimental Satellite on Electromagnetism Monitoring (ESEM) was proposed in 2003 and proved in 2013 after 10-years' scientific demonstration. The ESEM mission was proposed to be the first satellite of space-based geophysical fields observation system in China with a lot of application prospects in earthquake science, geophysics, space sciences and so on. And coincide with the mission objectives, the satellite decides to use the Circular Sun Synchronous Orbit with an altitude of 507km and descending node time at 14:00LT. The payload assemble includes 8 instruments, Search-Coil Magnetometer, Electric Field Detector, High precision Magnetometer, GNSS occupation Receiver, Plasma Analyzer, Langmuir Probe, Energetic Particle Detector, and Three-frequency Transmitter. According to the planned schedule, the satellite is due to be launched in 2016-2017 and will be onboard operated for 5 years.

关 键 词:Experimental  satellite    Electromagnetism  monitoring    Ionospheric  perturbation    Space  segment    Ground  segment
收稿时间:2014-04-23

The Experimental Satellite on Electro-magnetism Monitoring
Shen Xuhui.The Experimental Satellite on Electromagnetism Monitoring[J].Chinese Journal of Space Science,2014,34(5):558-562.
Authors:SHEN Xuhui
Institution:Institute of Earthquake Science, China Earthquake Administration, Beijing 100036
Abstract:The Experimental Satellite on Electromagnetism Monitoring (ESEM) was proposed in 2003 and proved in 2013 after 10-years' scientific demonstration. The ESEM mission was proposed to be the first satellite of space-based geophysical fields observation system in China with a lot of application prospects in earthquake science, geophysics, space sciences and so on. And coincide with the mission objectives, the satellite decides to use the Circular Sun Synchronous Orbit with an altitude of 507km and descending node time at 14:00LT. The payload assemble includes 8 instruments, Search-Coil Magnetometer, Electric Field Detector, High precision Magnetometer, GNSS occupation Receiver, Plasma Analyzer, Langmuir Probe, Energetic Particle Detector, and Three-frequency Transmitter. According to the planned schedule, the satellite is due to be launched in 2016-2017 and will be onboard operated for 5 years. 
Keywords:Experimental satellite  Electromagnetism monitoring  Ionospheric perturbation  Space segment  Ground segment
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