论文标题
辐射损伤退火的温度依赖性
Temperature dependence of radiation damage annealing of Silicon Photomultipliers
论文作者
论文摘要
在过去的十年中,越来越多地看到使用了硅光电塑料(SIPM)而不是光电倍增管(PMTS)。这是由于前者在后者上的各种优势,例如较小的尺寸,较低的工作电压,较高的检测效率,对磁场不敏感性以及发射振动的机械鲁棒性。所有这些功能使SIPM非常适合在基于太空的实验中使用,其中探测器需要紧凑,轻巧且能够幸存下来的发射条件。在空间条件下使用这种新型检测器的缺点是其对辐射损伤的敏感性。为了了解太空中sipm的寿命,必须研究由于辐射以及随后的恢复或退火而造成的损害。在这里,我们介绍了Hamamatsu S13360系列中三种不同类型的SIPMS的研究。在典型的任务中,在低地球轨道中维持相当于2年的辐射后,它们的行为均已提出,以及在不同条件下存储的过程中恢复这些探测器。存储条件的温度以及操作电压各不相同。研究发现,退火显着取决于检测器的温度,而在高温下储存的探测器的恢复速度明显更快,并且恢复了接近原始性能。此外,观察到合理偏置电压对退火没有显着影响。最后,将呈现退火速率作为温度的函数,以及针对未来SIPM基于SIPM的天体物理检测器Polar-2以及未来基于SIPM的空间传播任务的各种操作策略。
The last decade has increasingly seen the use of silicon photomultipliers (SiPMs) instead of photomultiplier tubes (PMTs). This is due to various advantages of the former on the latter like its smaller size, lower operating voltage, higher detection efficiency, insensitivity to magnetic fields and mechanical robustness to launch vibrations. All these features make SiPMs ideal for use on space based experiments where the detectors require to be compact, lightweight and capable of surviving launch conditions. A downside with the use of this novel type of detector in space conditions is its susceptibility to radiation damage. In order to understand the lifetime of SiPMs in space, both the damage sustained due to radiation as well as the subsequent recovery, or annealing, from this damage have to be studied. Here we present these studies for three different types of SiPMs from the Hamamatsu S13360 series. Both their behaviour after sustaining radiation equivalent to 2 years in low earth orbit in a typical mission is presented, as well as the recovery of these detectors while stored in different conditions. The storage conditions varied in temperature as well as in operating voltage. The study found that the annealing depends significantly on the temperature of the detectors with those stored at high temperatures recovering significantly faster and at recovering closer to the original performance. Additionally, no significant effect from a reasonable bias voltage on the annealing was observed. Finally the annealing rate as a function of temperature is presented along with various operating strategies for the future SiPM based astrophysical detector POLAR-2 as well as for future SiPM based space borne missions.