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适用范围:
This standard specifies the purpose, principle, requirements and method of spacecraft performance test under ambient pressure and thermal environment.
This standard is applicable to the performance tests of spacecraft or its cabin and large assemblies under ambient pressure and thermal environment, including integrated thermal test for sealed cabin, thermal deformation test under ambient pressure, separation and deployment test under ambient pressure and thermal environment, and can serve as a reference for the thermal performance tests of other large assemblies.
This standard is applicable to the performance tests of spacecraft or its cabin and large assemblies under ambient pressure and thermal environment, including integrated thermal test for sealed cabin, thermal deformation test under ambient pressure, separation and deployment test under ambient pressure and thermal environment, and can serve as a reference for the thermal performance tests of other large assemblies.
标准号:
GB/T 38201-2019e
标准名称:
航天器常压热性能试验方法
英文名称:
Performance test method for spacecraft under ambient pressure and thermal environment标准状态:
现行-
发布日期:
2019-10-18 -
实施日期:
2020-05-01 出版语种:
英文
起草人:
起草单位:
归口单位:
SAC/TC 425(Technical Committee on National Aerospace Technology and Application Standardization Administration of China).提出部门:
SAC/TC 425(Technical Committee on National Aerospace Technology and Application Standardization Administration of China).发布部门:
State Administration for Market Regulation and Standardization Administration of the People's Republic of China
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