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车轮静电光谱仪的性能描述

Characterizing the Performance of the Wheel Electrostatic Spectrometer
作者:Johansen, M. R.Mackey, P. J.Holbert, E.Calle, C. I.Clements, J. S. 作者单位:National Aeronautics and Space Administration, Cocoa Beach, FL. John F. Kennedy Space Center. 加工时间:2014-05-21 信息来源:科技报告(NASA) 索取原文[9 页]
关键词:传感器;静电学;绝缘子;分光仪
摘 要:Insulators need to be discharged after each wheel revolution. Sensor responses repeatable within one standard deviation in the noise of the signal. Insulators may not need to be cleaned after each revolution. Parent Technology-Mars Environmental Compatibility Assessment/Electrometer Electrostatic sensors with dissimilar cover insulators Protruding insulators tribocharge against regolith simulant Developed for use on the scoop for the 2001 Mars Odyssey lander Wheel Electrostatic Spectrometer Embedded electrostatic sensors in prototype Martian rover wheel If successful, this technology will enable constant electrostatic testing on Mars Air ionizing fan used to neutralize the surface charge on cover insulators. WES rolled on JSClA lunar simulant Control experiment-Static elimination not conducted between trials-Capacitor discharged after each experiment Charge neutralization experiment-Static elimination conducted between trials-Capacitor discharged after each experiment. Air ionizing fan used on insulators after each wheel revolution Capacitor discharged after each trial Care was taken to roll WES with same speed/pressure Error bars represent one standard deviation in the noise of each sensor.
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