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首页> 外文期刊>Journal of instrumentation: an IOP and SISSA journal >Prototype readout system for a multi Mpixels UV single-photon imaging detector capable of space flight operation
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Prototype readout system for a multi Mpixels UV single-photon imaging detector capable of space flight operation

机译:用于多重MPIXELS UV单光子成像检测器的原型读数系统,能够进行空间飞行运行

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摘要

Our collaboration works on the development of a large aperture, high resolution, UV single-photon imaging detector, funded through NASA's Strategic Astrophysics Technology (SAT) program. The detector uses a microchannel plate for charge multiplication, and orthogonal cross strip (XS) anodes for charge readout. Our target is to make an advancement in the technology readiness level (TRL), which enables real scale prototypes to be tested for future NASA missions. The baseline detector has an aperture of 50×50mm and requires 160 low-noise charge-sensitive channels, in order to extrapolate the incoming photon position with a spatial resolution of about 20 μm FWHM. Technologies involving space flight require highly integrated electronic systems operating at very low power. We have designed two ASICs which enable the construction of such readout system. First,a charge sensitive amplifier (CSAv3) ASIC provides an equivalent noise charge (ENC) of around 600 e~-, and a baseline gain of 10 mV/fC. The second, a Giga Sample per Second (GSPS) ASIC,called HalfGRAPH, is a 12-bit analog to digital converter. Its architecture is based on waveform sampling capacitor arrays and has about 8 μs of analog storage memory per channel. Both chips encapsulate 16 measurement channels. Using these chips, a small scale prototype readout system has been constructed on a FPGA Mezzanine Board (FMC), equipped with 32 measurement channels for system evaluation. We describe the construction of HalfGRAPH ASIC, detector's readout system concept and obtained results from the prototype system. As part of the space flight qualification,these chips were irradiated with a Cobalt gamma-ray source, to verify functional operation under ionizing radiation exposure.
机译:我们的协作工作是通过NASA的战略天体物理技术(SAT)计划资助的大孔径,高分辨率,UV单光子成像探测器的发展。检测器使用用于电荷乘法的微通道板,以及用于电荷读出的正交交叉条(XS)阳极。我们的目标是在技术准备水平(TRL)中提升,这使得能够为未来的美国航空航天局任务进行真正的规模原型。基线检测器的孔径为50×50mm,并且需要160个低噪声电荷敏感通道,以便将进入光子位置外推,空间分辨率为约20μmfwhm。涉及太空飞行的技术需要高功率运行的高度集成的电子系统。我们设计了两种ASIC,可实现这种读数系统的构建。首先,充电敏感放大器(CSAV3)ASIC提供约600 e〜 - - 和10mV / Fc的基线增益的等效噪声电荷(ENC)。第二,每秒GIGA样本(GSP)ASIC,称为半导体,是12位模数转换器。其架构基于波形采样电容阵列,每个通道具有大约8μs的模拟存储存储器。两个芯片都封装了16个测量通道。使用这些芯片,在FPGA夹层板(FMC)上建造了一个小型原型读数系统,配备了32个测量通道,用于系统评估。我们描述了探测器的探测器的读数系统概念和原型系统的结果。作为空间飞行资格的一部分,这些芯片用钴γ射线源照射,以验证电离辐射暴露下的功能性操作。

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