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A hot film anemometer for the Martian atmosphere

机译:火星大气热膜风速仪

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摘要

A novel design of a wind sensor for the surface of Mars is described. This sensor is to be included in the Rover Environment Monitoring Station (REMS) to be launched as a part of the Mars Science Laboratory in 2009. A 2D hot film anemometer composed of four hot points and a reference point has been conceived and implemented in the preliminary design model. It uses a closed thermal feedback loop based on thermal sigma-delta modulation. In this paper, the first results obtained in a Mars-like environment are shown, and indicate that sensitivities are expected to be in the range of 0.5 m/s and 10° in wind speed and direction.
机译:描述了一种用于火星表面的风传感器的新颖设计。该传感器将包括在火星科学实验室将于2009年启动的流浪者环境监测站(REMS)中。已经设计并实施了由四个热点和一个参考点组成的2D热膜风速仪。初步设计模型。它使用基于热sigma-delta调制的闭合热反馈环路。在本文中,显示了在类似火星的环境中获得的第一个结果,表明在风速和风向方面,灵敏度预计在0.5 m / s到10°的范围内。

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