美国军用标准航天器试验基线与量级调整研究  

Space Vehicle Test Baseline and Level Adjustment of US Military Standard

作　　者：李西园[1,2] 贾瑞金 孙雪吟[1] 尚永红 孙玉玮[1] 裴一飞[1] 王晶[1,3] LI Xi-yuan;JIA Rui-jin;SUN Xue-yin;SHANG Yong-hong;SUN Yu-wei;PEI Yi-fei;WANG Jing(Beijing Institute of Spacecraft Environment Engineering,Beijing 100094,China;Beihang University,Beijing 100191,China;Science and Technology on Reliability and Environmental Engineering Laboratory,Beijing 100094,China)

机构地区：[1]北京卫星环境工程研究所,北京100094 [2]北京航空航天大学,北京100191 [3]可靠性与环境工程技术重点实验室,北京100094

出　　处：《装备环境工程》2020年第5期87-94,共8页Equipment Environmental Engineering

摘　　要：对美国航天器试验的军用标准的发展进行了调研,系统地整理了MIL-STD-1540标准到SMC-S-016A标准的发展脉络,针对系统级、组件级试验基线的修订进行了整理、分析。以热试验为典型研究对象,整理了不同标准对于系统级、组件级热试验在试验温度范围、循环数、剪裁方法上的修改,对比了试验基线、试验量级的变迁,结合美国航天器型号与验证理念的发展,分析了其修订的依据,为我国相应标准的制定、修订提供了参考。The development of military standards for spacecraft test in the United States was investigated. The development of MIL-STD-154 standard to SMC-S-016 A standard was systematically sorted out. The revision of system level and component level test baseline was sorted out and analyzed. Taking the thermal test as a typical research object, the modification of different standards for the system level and component level thermal test in the test temperature range, cycle number and tailoring method were sorted out, the changes of test baseline and test level were compared, and the basis for revision was analyzed in combination with the development of spacecraft model and verification concept in the United States. It provides a reference for the formulation and revision of corresponding standards in China.

关 键 词：美国军用标准 航天器试验 MIL-STD-1540 SMC-S-016 基线 量级 剪裁 

分 类 号：V416[航空宇航科学与技术—航空宇航推进理论与工程]