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Tiny Ionospheric Photometers on FORMOSAT-3/COSMIC: On-orbit performance

机译:FORMOSAT-3 / COSMIC上的微型电离光度计:在轨性能

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The Tiny Ionospheric Photometer (TIP) sensors aboard the Constellation Observing System for Meterology, Ionosphere and Climate (COSMIC, also called FORMOSAT-3) spacecraft comprise a suite of six nadir-viewing ultraviolet photometers for characterizing the Earth's nightside ionosphere. The TIP instruments complement the ionospheric capabilities of the GPS occultation experiment (GOX) by characterizing horizontal ionospheric density gradients. These photometers target 01 135.6 nm emission produced by ionospheric O~++e recombination and measure ionospheric structure with a spatial resolution of 10-30 km. The TIP instrument design had to solve several design challenges in order to achieve its intended science and mission requirements within operational constraints imposed by the spacecraft and budget constraints. The photometers have a simple design which excludes OI 130.4 nm emission and achieves a sensitivity of approximately 500 counts/s/Rayleigh at 135.6nm. The satellites initially orbited in the same plane at 500 km, then over the course of 13 months they were individually raised to their final 800 km orbits in six planes separated by 24° in right ascension. These maneuvers provided opportunities for cross-calibration among the sensors, for multipass observations as the satellites orbit together early in the mission, and for observations at different spatial resolutions as the spacecraft operate at different altitudes. In this paper we evaluate on-orbit sensor performance of the TIP sensors, and discuss improvements for follow-on missions.
机译:星座计量学,电离层和气候星座观测系统(COSMIC,也称为FORMOSAT-3)上的微型电离层光度计(TIP)传感器包括一套六套天底观测紫外光度计,用于表征地球的夜间电离层。 TIP仪器通过表征水平电离层密度梯度来补充GPS掩星实验(GOX)的电离层能力。这些光度计的目标是电离层O〜++ e重组产生的01 135.6 nm发射,并以10-30 km的空间分辨率测量电离层结构。 TIP仪器的设计必须解决几个设计难题,才能在航天器施加的运行限制和预算限制内达到预期的科学和任务要求。光度计具有简单的设计,可排除130.4 nm的OI发射,并在135.6nm处获得约500个计数/秒/瑞利的灵敏度。卫星最初在同一平面上以500 km的轨道运行,然后在13个月的过程中,它们分别在六架以24°右仰角分开的平面中分别升至最后800 km轨道。这些演习为传感器之间的相互校准,在任务初期卫星一起轨道飞行时进行多程观测以及在航天器以不同高度运行时以不同空间分辨率进行观测提供了机会。在本文中,我们评估了TIP传感器在轨传感器的性能,并讨论了后续任务的改进。

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