Magnetic Field Experiment on Yinghuo-1 at Mars Hua Zhao, G. W. Zhu, J. D. Wang, M. F. Yu, L. Li, Y. Q. Sun, S. W. Chen, H. Z. Liao, and B. Zhou Center for Space Science and Applied Research (CSSAR), Chinese Academy of Sciences, Beijing, China Abstract: A micro-satellite, Yinghuo-1, would be launched with Phobos-Grunt in October, 2009 to investigate the space environment around Mars. YH-1 and Phobos-Grunt forms a twopoint measurement configuration in the Martian space environment, and equipped with similar magnetic field and plasma detecting payload on two spacecraft would give some coordinated exploration around Mars. YH-1 would orbit Mars with periapsis of 800 km above the Martian surface, and apoapsis about 80000 km to the center of Mars. The orbit inclination is in the range of 0—7o to the Martian equator. A flux-gate type magnetometer, with two sensors, is developed for YH-1 spacecraft. Two sensors are mounted on one-side of the deployable solar panel with a radial separation about 45 cm to function as a gradiometer to minimize the affects of platform remanence. The dynamic range of √ magnetometer is with a 16-bit ADC converter, and the the noise level is better than 0.01 nT/ Hz, to measure three-component magnetic field from DC to 10Hz. Flux-gate magnetometer would work together with the Plasma Package onboard of YH-1 to investigate the Martian bow shock, magnetosheath, magnetic pileup region (MPR). A detail description of the flux-gate magnetometer is presented in this paper, with some test and calibration results.
37th COSPAR Scientific Assembly
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