首页> 外文期刊>Microelectronics & Reliability >Failure rate calculation method for high power devices in space applications at low earth orbit
【24h】

Failure rate calculation method for high power devices in space applications at low earth orbit

机译:低地球轨道空间应用中大功率设备的失效率计算方法

获取原文
获取原文并翻译 | 示例
           

摘要

This paper discusses the universal calculation method for space proton induced failure rate on high power device. High energetic particles can be the reason of power device failure in both terrestrial and space. T-CAD simulation result gives a threshold charge value for the device destruction which is triggered by energetic proton from space. The amount of threshold charge depends on applied voltage for high power device. The probability of charge generation in silicon due to proton penetration is considered as well. This probability function variation depends on the thickness of device and incident energy of proton which studied before at there. Last consideration on this paper is 33 kV PiN diode's Single Event Upset Cross section and failure rate which was calculated by proposed method in Low earth orbit environment condition. (C) 2016 Elsevier Ltd. All rights reserved.
机译:本文讨论了大功率装置上空间质子引起的失效率的通用计算方法。高能粒子可能是地面和太空中功率设备故障的原因。 T-CAD仿真结果给出了设备破坏的阈值电荷值,该阈值电荷是由来自太空的高能质子触发的。阈值电荷的数量取决于大功率设备的施加电压。还考虑了由于质子渗透而在硅中产生电荷的可能性。这种概率函数的变化取决于器件的厚度和之前研究过的质子的入射能。本文最后要考虑的是33 kV PiN二极管的单事件翻转截面和失效率,这是通过在低地球轨道环境条件下提出的方法计算得出的。 (C)2016 Elsevier Ltd.保留所有权利。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号