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Proton loss of inner radiation belt during geomagnetic storm of 2018 based on CSES satellite observation 被引量:1
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作者 Zhen-Xia Zhang xu-hui shen +1 位作者 Xin-Qiao Li Yong-Fu Wang 《Chinese Physics B》 SCIE EI CAS CSCD 2021年第12期664-670,共7页
The proton distribution in inner radiation belt is often affected by strong geomagnetic storm disturbance.Based on the data of the sun-synchronous CSES satellite,which carries with several high energy particle payload... The proton distribution in inner radiation belt is often affected by strong geomagnetic storm disturbance.Based on the data of the sun-synchronous CSES satellite,which carries with several high energy particle payloads and was launched in February 2018,we analyzed the extensive proton variations in the inner radiation belt in a wide energy range of 2 MeV-220 MeV during 2018 major geomagnetic storm.The result indicates that the loss mechanism of protons was energy dependence which is consistent with some previous studies.For protons at low energy 2 MeV-20 MeV,the fluxes were decreased during main phase of the storm and did not come back quickly during the recovery phase,which is likely to be caused by Coulomb collision due to neutral atmosphere density variation.At higher energy 30 MeV-100 MeV,it was confirmed that the magnetic field line curvature scattering plays a significant role in the proton loss phenomenon during this storm.At highest energies>100 MeV,the fluxes of protons kept a stable level and did not exhibit a significant loss during this storm. 展开更多
关键词 proton loss the inner radiation belt CSES satellite field line curvature scattering
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Preliminary proposal of scientific data verification in CSES mission
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作者 Lan-wei Wang xu-hui shen +1 位作者 Yu Zhang Rui Yan 《Earthquake Science》 CSCD 2015年第4期303-310,共8页
China Seismo-Electromagnetic Satellite (CSES) will be launched at the end of 2016 and the orbit is sun- synchronous and the altitude is about 500 km. The design of CSES satellite and ground segment are introduced in... China Seismo-Electromagnetic Satellite (CSES) will be launched at the end of 2016 and the orbit is sun- synchronous and the altitude is about 500 km. The design of CSES satellite and ground segment are introduced in this paper first. And then the preliminary proposals of scientific data verification and cross-verification in CSES mission are given, which can be used to classify the payloads' operation state, and validate the reliability of data. 展开更多
关键词 CSES mission Data verification Inter-calibration
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