Abstract
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.
General information
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Status: Under development
You can help develop this draft international standard by contacting your national member
Stage: DIS ballot initiated: 12 weeks [40.20] -
Edition: 1Number of pages: 27
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Technical Committee :ISO/TC 20/SC 14ICS :49.140
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