Stray Light Analysis and Testing of the SoloHI (Solar Orbiter Heliospheric Imager) and WISPR (Wide Field Imager for Solar Probe) Heliospheric Imagers

被引:5
|
作者
Thernisien, Arnaud F. R. [1 ]
Howard, Russell A. [1 ]
Korendyke, Clarence [1 ]
Carter, Tim [1 ]
Chua, Damien [1 ]
Plunkett, Simon [1 ]
机构
[1] US Naval Res Lab, 4555 Overlook Ave SW, Washington, DC 20375 USA
来源
SPACE TELESCOPES AND INSTRUMENTATION 2018: OPTICAL, INFRARED, AND MILLIMETER WAVE | 2018年 / 10698卷
关键词
Stray light modeling; solar corona; Solar Orbiter; Parker Solar Probe; heliospheric imager; flight model testing; stray light testing; MISSION;
D O I
10.1117/12.2313645
中图分类号
P1 [天文学];
学科分类号
0704 ;
摘要
The techniques for stray light analysis, optimization and testing are described for two space telescopes that observe the solar corona: the Solar Orbiter Heliospheric Imager (SoloHI) that will fly on the ESA Solar Orbiter (SolO), and the Wide Field Imager for Solar Probe (WISPR) that will fly on the NASA Parker Solar Probe (PSP) mission. Imaging the solar corona is challenging, because the corona is six orders of magnitude dimmer than the Sun surface at the limb, and the coronal brightness continues to decrease to ten orders of magnitude below the Sun limb above 5 degrees elongation from Sun center. The SoloHI and WISPR instruments are located behind their respective spacecraft heat shield. Each spacecraft heat shield does not block the instrument field of view above the solar limb, but will prevent direct sunlight entering the instrument aperture. To satisfy the instrument stray light attenuation required to observe the solar corona, an additional set of instrument baffles were designed and tested for successive diffraction of the heat shield diffracted light before entering the telescope entrance pupil. A semi empirical model of diffraction was used to design the baffles, and tests of the flight models were performed in flight like conditions with the aim of verifying the rejection of the design. Test data showed that the baffle systems behaved as expected. A second source of stray light is due to reflections of the sunlight off of the spacecraft structures and towards the instruments. This is especially the case for SoloHI where one of the spacecraft 8m tall solar arrays is located behind the telescope and reflects sunlight back onto the instrument baffles. The SoloHI baffle design had to be adjusted to mitigate that component, which was achieved by modifying their geometry and their optical coating. Laboratory tests of the flight model were performed. The test data were correlated with the predictions of a ray tracing model, which enabled the fine tuning of the model. Finally, end-to-end ray tracing was used to predict the stray light for the flight conditions.
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页数:19
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