该文系统梳理国外宇航机构航天器太阳翼研制标准及试验验证体系,重点分析其研制阶段的试验项目构成。通过对比美国军用标准MIL-STD-1540E与欧洲航天标准化合作组织（ECSS）标准ECSS-E-10-03A在太阳翼试验项目设置及技术指标要求方面的异同,揭示两套标准的共性与差异。研究成果为中国航天器太阳翼研制流程优化与验证体系构建提供可操作的参考依据。
Abstract
This study systematically reviews international aerospace standards and test-verification frameworks for spacecraft solar arrays, with particular focus on test item configurations during the development phase. By comparing the test item specifications and technical requirement criteria of the U.S. Military Standard MIL-STD-1540E and the European Cooperation for Space Standardization （ECSS） standard ECSS-E-10-03A, the study reveals commonalities and discrepancies between the two standards. The findings provide an actionable reference for optimizing China’s spacecraft solar array development processes and establishing robust verification systems.
关键词
航天器 /
太阳电池阵 /
研制标准 /
试验验证 /
研制流程
Key words
spacecraft /
solar array /
development standards /
test verification /
development process
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