Automatic Control System of Thermal-vacuum-testing
Spacecraft thermal-vacuum test chamber automation (600 m³, ±150 °C, 750+ test points, 2000+ parameters, 720+ hr continuous operation).
Technical specifications
- Purpose
- Automatic control of spacecraft thermal-vacuum testing in vacuum chamber; off-nominal situation analysis
- Year of release
- 2011
- Guaranteed service life, years
- 5
- Estimated production/delivery time
- 12 months
- Customization
- Can be adapted to customer requirements
- Vacuum chamber temperature range, °C
- ±150
- Duration of continuous tests without failing, hours
- >720
- Volume of horizontal vacuum chamber, m³
- 600
- Number of product test points
- >750
- Number of controlled parameters
- >2000
- TRL
- 9
About
The Automatic Control System of Thermal-vacuum-testing provides automatic control of thermal vacuum testing of spacecraft in a vacuum chamber and analyzes off-nominal situations. It controls a 600 m³ horizontal vacuum chamber across ±150 °C, monitoring more than 750 product test points and more than 2000 controlled parameters. Continuous test duration without failures exceeds 720 hours. Released in 2011 with 5-year service life and 12-month delivery time. Adaptable to customer requirements.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.
