航天器常压热性能试验方法

Performance test method for spacecraft under ambient pressure and thermal environment

标准介绍

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.

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