首页 | 本学科首页   官方微博 | 高级检索  
     检索      

星载大功率GaN固态功放寿命评估方法
引用本文:敬小东,王海龙,游飞,魏彦江,钟世昌.星载大功率GaN固态功放寿命评估方法[J].航天器环境工程,2021,38(4):420-425.
作者姓名:敬小东  王海龙  游飞  魏彦江  钟世昌
作者单位:西南电子设备研究所,成都 610036;电子科技大学 电子科学与工程学院,成都 611731;四川省宽带微波电路高密度集成工程研究中心,成都 610036;西南电子设备研究所,成都 610036;四川省宽带微波电路高密度集成工程研究中心,成都 610036;电子科技大学 电子科学与工程学院,成都 611731;南京电子器件研究所,南京 210016
摘    要:近年来大功率氮化镓(GaN)固态功放开始逐步星载应用,但产品可靠性仍未得到充分验证.文章提出利用加速寿命试验(ALT)和在轨工作情况相结合的方法进行大功率GaN固态功放寿命评估.首先利用故障模式、机理及影响分析(FMMEA)确定固态功放的薄弱环节和主要失效机理;然后基于阿仑尼乌斯(Arrhenius)模型研究加速寿命试...

关 键 词:氮化镓  固态功放  加速寿命试验  寿命评估
收稿时间:2020-12-04

Method for life evaluation of spaceborne high power GaN solid state power amplifier
Institution:1.Southwest China Research Institute of Electronic Equipment, Chengdu 610036, China2.School of Electronic Science and Engineering, University of Electronic Science and Technology of China, Chengdu 611731, China3.Sichuan Broadband Microwave Circuit High Density Integrated Engineering Research Center, Chengdu 610036, China4.Nanjing Electronic Devices Institute, Nanjing 210016, China
Abstract:In recent years, the high-power gallium nitride (GaN) solid-state power amplifiers (SSPA) have gradually been put into aerospace applications, but their reliability is still to be verified. This paper proposes a method for evaluating the lifetime of the high-power GaN SSPA through the accelerated life test (ALT), as well as their on-orbit working performance. First, the weakness and the main failure mechanisms of the GaN SSPA are analyzed, including the failure mode, mechanisms and effects analysis (FMMEA). Then, a method of determining the value of the activation energy and the accelerated stress is discussed, based on the Arrhenius model. At the same time, an ALT of 75 ℃ with a duration of 10 000 h is carried out. Finally, based on the test results and the on-orbit performance, a series of deduced results are obtained under the normal working condition of 45 ℃ which illustrate that the mean time to failure (MTTF) is 1.26×106 h, while the failure rate is 7.93×10-7, and the working reliability of 15 years is 0.901.
Keywords:
本文献已被 CNKI 万方数据 等数据库收录!
点击此处可从《航天器环境工程》浏览原始摘要信息
点击此处可从《航天器环境工程》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号