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Ground Test Results of the Micro-Vibration Interference for the X-Ray Microcalorimeter Onboard XRISM

Proceedings of SPIE--the International Society for Optical Engineering(2022)

Univ Tokyo | Ehime Univ | Japan Aerosp Explorat Agcy JAXA | NASA | Kanazawa Univ

Cited 1|Views24
Abstract
Resolve is a payload hosting an x-ray microcalorimeter detector operated at 50 mK in the X-Ray Imaging and Spectroscopy Mission (XRISM), which is currently under development by an international collaboration and is planned to be launched in 2023. One of the technical concerns is the micro-vibration interference to the sensitive microcalorimeter detector by the spacecraft bus components. We verified this in a series of the ground tests in 2021–2022, the results of which are reported here. We defined the micro-vibration interface between the spacecraft and the Resolve instrument. In the instrument-level test, we tested the flight-model hardware against the interface level by injecting micro-vibration using vibrators and evaluated the instrument response using the 50 mK stage temperature stability, the ADR magnet current consumption rate, and the detector noise spectra. We found the strong responses when injecting micro-vibration at ∼200, 380, and 610 Hz. In the former two cases, the beat among the injected frequency and the cryocooler frequency harmonics are also observed in the detector noise spectra. In the spacecraft-level test, we measured the acceleration and the instrument responses with and without suspending the entire spacecraft. The reaction wheels and the inertial reference units, two major sources of micro-vibration among the bus components, were operated. We found that the observed Resolve responses are within acceptable levels.
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low temperature detector,x-ray microcalorimeter,micro-vibration interference,XRISM
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要点】:本文报道了针对XRISM任务中X射线微热量计探测器在空间飞行器微振动干扰方面的地面测试结果,提出了一种评估和降低干扰的创新方法。

方法】:通过在仪器级测试中使用振动器注入微振动,并利用50 mK舞台温度稳定性、ADR磁铁电流消耗率和探测器噪声频谱评估仪器响应,定义了空间飞行器与 Resolve 设备之间的微振动接口。

实验】:在2021-2022年进行的一系列地面实验中,使用 flight-model 硬件,发现注入微振动在约200、380和610 Hz时仪器有强烈反应,且在探测器噪声频谱中观察到注入频率与制冷机频率谐波之间的拍频;在飞行器级测试中,通过操作反应轮和惯性参考单元,测量了有无悬挂整个飞行器时的加速度和仪器响应,结果均在可接受范围内。