Automatic Control System of Thermal-vacuum-testing
Automatic control system of thermal-vacuum-testing for spacecraft.
Technical specifications
- Vacuum chamber temperature range
- ±150 C
- Duration of continuous tests without failing
- >720 hours
- Volume of the horizontal vacuum chamber, m3
- 600
- Number of product test points
- more than 750
- Number of controlled parameters
- more than 2000
About
Automatic control system of thermal-vacuum-testing for spacecraft.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.