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Rocket-borne instrument to detect charged smoke and cloud particles in the mesospheric region

机译:Rocket-Borne仪器以检测在Mesompheric地区的带电烟雾和云颗粒

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Summary form only given. A design of an instrument is described that is capable of detecting charged sub-visible particles in the upper atmosphere. The instrument is placed at the top of a sounding rocket with a /spl sim/20 cm/sup 2/ entrance slit. The sampled air flows between three pairs of graphite patch electrodes placed one above another, and connected to sensitive electrometers. The pairs of electrodes are biased symmetrically and the bias potential increases downward. The static electric field allows the charge- and mass-selective collection. The first pair of electrodes captures the electrons and light ions. Heavier ions within a mass range of 100-1000 amu are collected on the second pair and smoke particles or heavy cluster ions up to 10000 amu are collected on the third pair. The design of the detector has been optimized with a consideration to the possible coning motion of the rocket, collection efficiency, and gas flow dynamics. Numerical Monte Carlo and Direct Simulation codes were used to study the effect of collisions. The results show that above 50 km collisions with neutrals have only a small effect on the detector performance and that vacuum pumping is not required.
机译:摘要表格仅给出。描述了一种仪器的设计,其能够检测高层大气中的带电的亚可见颗粒。仪器放置在带有/ SPL SIM / 20 cm / sup 2 /入口狭缝的发声火箭顶部。采样的空气在另一个放置在另一个上方的石墨贴片电极之间,并连接到敏感电电动机。一对电极对称偏置,偏置电位向下增加。静电场允许充电和质量选择性收集。第一对电极捕获电子和光离子。在第三对中收集100-1000AMU的质量范围内的较重离子,并在第三对中收集高达10000 AMU的烟雾颗粒或重簇离子。已经考虑到火箭,收集效率和气流动力学的可能对照运动来优化检测器的设计。使用数值蒙特卡罗和直接仿真代码来研究碰撞的影响。结果表明,与中性的50公里碰撞仅对探测器性能产生小效果,并且不需要真空泵。

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