Instrument overview of the Swift Solar Activity X-ray Imager (SSAXI-Rocket)

The Swift Solar Activity X-Ray Imager (SSAXI-Rocket) sounding rocket experiment is a direct-imaging, soft Xray telescope optimized for the observation of large (GOES C class-X class) solar flares. SSAXI-Rocket has high temporal sampling cadence (&gt; 5 Hz) enabled by a fast-readout CMOS detector. A single Wolter-1 optic focuses light onto the detector plane. The optic has a 15.8′′ half-power diameter (HPD) angular resolution on-axis and an effective area of 0.64 cm<sup>2</sup> at 4.5 keV. The SSAXI-Rocket camera reads out a spectrally integrated signal, and the system spatial resolution is designed to be &lt; 16′′ HPD over the instrument field of view (&gt; 55′ × 55′). The detector is a back-illuminated delta doped CMOS (2048 × 2048 pixels) with 10 &mu;m pitch pixels. This manuscript details our instrument design, and overviews the processes employed in telescope alignment, testing, delivery, and integration onto the Hi-C Sounding Rocket. We present the “as-built” projected flight performance of the delivered SSAXI-Rocket flight system, obtained by synthesizing the results of pre-flight subsystem testing and measurements performed during system integration and alignment.

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Published
2024-08-21
DOI
https://doi.org/10.1117/12.3020753
Primary Topic
Solar and Space Plasma Dynamics
Type
article
Field-Weighted Citation Impact
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article

Instrument overview of the Swift Solar Activity X-ray Imager (SSAXI-Rocket)

Johnny Ho, K. G. McCracken, Suzanne Romaine, Edward Hertz et al.
Solar and Space Plasma Dynamics
article

Instrument overview of the Swift Solar Activity X-ray Imager (SSAXI-Rocket)

Johnny Ho, K. G. McCracken, Suzanne Romaine, Edward Hertz, Thomas Gauron, D. Caldwell, Sophia A. Sánchez-Maes, Isaac Anderson, A. Kenter, Elias Aguirre-Contreras, Gabriel Dubinski, Christopher Moore, Jae Sub Hong
article en

Abstract

The Swift Solar Activity X-Ray Imager (SSAXI-Rocket) sounding rocket experiment is a direct-imaging, soft Xray telescope optimized for the observation of large (GOES C class-X class) solar flares. SSAXI-Rocket has high temporal sampling cadence (&gt; 5 Hz) enabled by a fast-readout CMOS detector. A single Wolter-1 optic focuses light onto the detector plane. The optic has a 15.8′′ half-power diameter (HPD) angular resolution on-axis and an effective area of 0.64 cm<sup>2</sup> at 4.5 keV. The SSAXI-Rocket camera reads out a spectrally integrated signal, and the system spatial resolution is designed to be &lt; 16′′ HPD over the instrument field of view (&gt; 55′ × 55′). The detector is a back-illuminated delta doped CMOS (2048 × 2048 pixels) with 10 &mu;m pitch pixels. This manuscript details our instrument design, and overviews the processes employed in telescope alignment, testing, delivery, and integration onto the Hi-C Sounding Rocket. We present the “as-built” projected flight performance of the delivered SSAXI-Rocket flight system, obtained by synthesizing the results of pre-flight subsystem testing and measurements performed during system integration and alignment.

Vol. 289
Center for Astrophysics Harvard & Smithsonian (US)
National Science Foundation, National Aeronautics and Space Administration, John Templeton Foundation, California Institute of Technology, Nuclear Safety and Security Commission, Jet Propulsion Laboratory, Heliophysics Division
Affordable and clean energy
Openalex Percentile: Top 89%
Solar and Space Plasma Dynamics
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