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Research of thermal cycles of long wavelength MCT infrared detectors

机译:长波长MCT红外探测器的热循环研究

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The conflict of longevity of satellite's service and limited life of Sterling cooler decides that coolers should work on the intermittent mode in space. As a result, The HgCdTe (MCT) infrared (IR) detectors in satellite are commonly subjected to thousands of repeated thermal cycles from below -173°C to room temperature (20°C), which brings some new reliability problems. Especially the mismatch of coefficient of thermal expansion (CTE) of different materials may lead to some unfamiliar failure modes with such low temperature and nearly 200°C span of thermal cycles. In order to study the characteristics of MCT detectors under the stress of thermal cycles, this paper introduced a special automatic system. The system is mainly composed of a sub-container of liquid nitrogen, a heater controlled by the PID hardware, and an object stage on which the MCT detectors to be tested are mounted. Furthermore, the sub-container, the heater and the stage are positioned in a large vacuum tank. In the course of thermal cycles, the object stage moved up and down with MCT detectors is driven by a step motor. When it rises to the bottom of liquid nitrogen sub-container, the stage is to be cooled with detectors, and when declines to the heater, the stage to be heated with detectors, too. At last, two long wavelength MCT detector samples are tested with this equipment, and the resistance, the signal and the noise are measured . It shows that all the pixels' resistance didn't change beyond 5% after 5000 cycles. However, the tested signal of the last pixel of both detectors increased sharply after 1000 cycles, and fell to normal level after 5000 cycles, with its noise altering a little from beginning to end. A deduction is given in this paper for this phenomenon. In accordance, the thermal cycle equipment and the experimental data, would supply some references to the design and fabrication of MCT IR detectors.
机译:卫星服务的寿命冲突和Sterling Cooler的有限生活决定了冷却器应该在空间中的间歇模式下工作。结果,卫星中的HGCDTE(MCT)红外(IR)探测器通常从低于-173°C至173°C的重复热循环到室温(20°C),这带来了一些新的可靠性问题。特别是不同材料的热膨胀系数(CTE)的不匹配可能导致一些不熟悉的衰竭模式,具有这种低温和近200°C的热循环跨度。为了研究热循环应力下MCT探测器的特性,本文介绍了一种特殊的自动系统。该系统主要由液氮的子容器组成,由PID硬件控制的加热器,以及安装有测试的MCT探测器的物体级。此外,子容器,加热器和级位于大型真空罐中。在热循环过程中,用MCT检测器向上移动的物体级由步进电机驱动。当它升到液氮子容器的底部时,舞台将用探测器冷却,并且当加热器下降时,也用探测器加热。最后,使用该设备测试两个长波长MCT检测器样本,测量电阻,信号和噪声。它表明,在5000个周期后,所有像素的阻力不会超过5%。然而,两个探测器的最后像素的测试信号在1000个周期后急剧增加,并且在5000周期后倒入正常水平,其噪音从头到尾改变了一点。本文为这一现象提供了扣除。根据,热循环设备和实验数据,将提供对MCT IR探测器的设计和制造的一些引用。

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