Development of x-ray optics for the solar flare sounding rocket FOXSI-4: ground calibration

We have been developing X-ray optics for a fourth FOXSI (Focusing Optics X-ray Solar Imager) sounding rocket experiment, FOXSI-4. We fabricated two types of X-ray optics, soft X-ray optics (SXR) and hard X-ray optics (HXR), specified for soft and hard X-ray observations. We conducted X-ray irradiation tests to evaluate X-ray performances such as angular resolution and effective area. For the Flight Model (FM) SXR, the resultant angular resolution in Half Power Diameter (HPD) is 16 ± 2 / 14 ± 2 arcseconds at 2.7 / 4.5 keV for the best images, respectively and no significant energy dependence in HPD is seen. The observed effective area was reproduced within an accuracy of 10% by using our original ray-tracing simulator considering all of the SXR components in the 1.5-16 keV range at the smallest off-axis angle. Subsequently, both FM mirror module assemblies were integrated into a sounding rocket in combination with detectors and the vibration tests were performed for the whole sounding rocket system. Finally, FOXSI-4 was successfully launched on April 17, 2024 (UTC), and the sounding rocket and the data were also recovered successfully.

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Publication Details

Published
2024-08-21
DOI
https://doi.org/10.1117/12.3018109
Primary Topic
Solar and Space Plasma Dynamics
Type
article
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article

Development of x-ray optics for the solar flare sounding rocket FOXSI-4: ground calibration

Noriyuki Narukage, Takahiro Saito, Kentarou Hiraguri, Naoki Ishida et al.
Solar and Space Plasma Dynamics
article

Development of x-ray optics for the solar flare sounding rocket FOXSI-4: ground calibration

Noriyuki Narukage, Takahiro Saito, Kentarou Hiraguri, Naoki Ishida, Kikuko Miyata, Yoichi Imamura, Gota Yamaguchi, Wataru Kato, Ikuyuki Mitsuishi, Yusuke Matsuzawa, Hirokazu Hashizume, Takehiro Kume, Hidekazu Mimura, Yusuke Yoshida, Kazuki Ampuku, Keitoku Yoshihira, Shunsuke Ito, Yoshitaka Inoue, Ryuto Fujii, Keisuke Tamura, Shutaro Mohri, Tetsuo Kano, Kumiko Okada, Koki Sakuta
article en

Abstract

We have been developing X-ray optics for a fourth FOXSI (Focusing Optics X-ray Solar Imager) sounding rocket experiment, FOXSI-4. We fabricated two types of X-ray optics, soft X-ray optics (SXR) and hard X-ray optics (HXR), specified for soft and hard X-ray observations. We conducted X-ray irradiation tests to evaluate X-ray performances such as angular resolution and effective area. For the Flight Model (FM) SXR, the resultant angular resolution in Half Power Diameter (HPD) is 16 ± 2 / 14 ± 2 arcseconds at 2.7 / 4.5 keV for the best images, respectively and no significant energy dependence in HPD is seen. The observed effective area was reproduced within an accuracy of 10% by using our original ray-tracing simulator considering all of the SXR components in the 1.5-16 keV range at the smallest off-axis angle. Subsequently, both FM mirror module assemblies were integrated into a sounding rocket in combination with detectors and the vibration tests were performed for the whole sounding rocket system. Finally, FOXSI-4 was successfully launched on April 17, 2024 (UTC), and the sounding rocket and the data were also recovered successfully.

Goddard Space Flight Center (US), Nitto RIKEN (Japan) (JP), National Astronomical Observatory of Japan (JP), Nagoya University (JP), University of Maryland, College Park (US), The University of Tokyo (JP), Meijo University (JP)
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Solar and Space Plasma Dynamics
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