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One mission devoted to detect the mechanism between Earth magnetosphere and solar wind is briefly introduced. Its orbit is an elliptic one with a perigee altitude of 6378km and an apogee altitude of 7*6378km. The space environment of such an orbit in space has seldom been probed. In order to carry out a successful mission, it is necessary to simulate some vital radiation characteristics in the space environment. some electronic devices and optical devices onboard the spacecraft are liable to be affected by the space environment, where solar wind might greatly influence the operation of spacecraft. The simulation results will give great supports to the devising the of the spacecraft and successful operation of the mission.
Hu Jiang andJinpei Yu
"Simulation of some vital space radiation characteristics for a magnetosphere probing mission", Proc. SPIE 10463, AOPC 2017: Space Optics and Earth Imaging and Space Navigation, 104630S (24 October 2017); https://doi.org/10.1117/12.2281175
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Hu Jiang, Jinpei Yu, "Simulation of some vital space radiation characteristics for a magnetosphere probing mission," Proc. SPIE 10463, AOPC 2017: Space Optics and Earth Imaging and Space Navigation, 104630S (24 October 2017); https://doi.org/10.1117/12.2281175