摘要
以环境工程理论为基础,研究了宇航元器件在装机条件下的热环境特点及其对元器件的影响,确立了热环境适应性验证试验项目、试验剖面与评价判据,提出了一套完整的宇航元器件热环境适应性评价方法。
Based on the environmental sensitive factors of space-borne components profiles and test criteria for evaluating the comprehensive method for the thermal borne components was proposed. engineering theory, the thermal environment and inside equipment were examined. The test items, test thermal environment adaptability were established. A environmental adaptability evaluation of space-borne components was proposed.
出处
《电子产品可靠性与环境试验》
2012年第3期6-10,共5页
Electronic Product Reliability and Environmental Testing
基金
国家重大工程专项(2009ZX01025-001-A601)资助
关键词
宇航元器件
热环境
环境适应性
评价技术
space-borne component
thermal environment
environmental adaptability
eval-uation
