2017
DOI: 10.1117/1.jatis.4.1.011205
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In-orbit operation of the soft x-ray spectrometer onboard the Hitomi satellite

Abstract: Abstract. We summarize all of the in-orbit operations of the soft x-ray spectrometer (SXS) onboard the ASTRO-H (Hitomi) satellite. The satellite was launched on February 17, 2016, and the communication with the satellite ceased on March 26, 2016. The SXS was still in the commissioning phase, in which the set-ups were progressively changed. This paper is intended to serve as a concise reference of the events in orbit in order to properly interpret the SXS data taken during its short lifetime and as a test case … Show more

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Cited by 7 publications
(5 citation statements)
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“…The SXS was commissioned shortly after launch and began making astronomical measurements 4 just days into the mission. 5 The instrument performed as expected until the untimely loss of the mission on March 26, 2016. The SXS microcalorimeter array 6 consisted of ion-implanted silicon thermistors and HgTe thermalizing x-ray absorbers that operate at a heat-sink temperature of 50 mK. Because of this low operating temperature, the optical path of the SXS included a set of five thin-film aluminized polyimide filters anchored to nested temperature stages.…”
Section: Introductionmentioning
confidence: 72%
See 1 more Smart Citation
“…The SXS was commissioned shortly after launch and began making astronomical measurements 4 just days into the mission. 5 The instrument performed as expected until the untimely loss of the mission on March 26, 2016. The SXS microcalorimeter array 6 consisted of ion-implanted silicon thermistors and HgTe thermalizing x-ray absorbers that operate at a heat-sink temperature of 50 mK. Because of this low operating temperature, the optical path of the SXS included a set of five thin-film aluminized polyimide filters anchored to nested temperature stages.…”
Section: Introductionmentioning
confidence: 72%
“…We intended to open the gate valve at the end of the commissioning phase, ∼40 days into the mission, when the spacecraft outgassing rate was predicted to have been low enough to avoid contamination of the dewar optical blocking filters. 5 The x-ray transmission of the Be Table 3 Absorber measurement summary. The absorbers are beveled such that the front surface is slightly larger than the back surface.…”
Section: Gate Valve Beryllium Windowmentioning
confidence: 99%
“…The shape of the Bremsstrahlung is a little different, but depends quite a bit on the exact match of the accelerating voltage (supposed to be 11. 3 kV, but which has some margin of error (about ±0.3 kV) for the measurements). In addition, the decrease of SDD efficiency due to the limited thickness of the silicon of the detector has not been taken into account.…”
Section: Model Validationmentioning
confidence: 94%
“…The SXS was still in the commissioning phase when Hitomi lost attitude control. The in-orbit operation of the SXS, including the operations of the power system, cooling system, and signal acquisition system, was a complete success [51]. For the cooling system to run detectors at 50 mK, the cooling chain worked successfully as mentioned above, and cooling is performed by the ADR and the temperature is kept within a few µ Kelvin by Proportional-Integral-Differential (PID) control in orbit [9].…”
Section: Gain Correction and Line Spread Functionmentioning
confidence: 99%