The standard specifies the technical requirements for the control of environmental parameters in the whole process of spacecraft system level assembly, integration and test.
The standard is applicable to the spacecraft system level assembly, integration, and test.
PROJECT
ISO/DIS 25339
40.20
DIS ballot initiated: 12 weeks
Jul 24, 2026
To view the full content, you need to register or to log in to your account by clicking on the "Log in" button