Technical Condition Monitoring System
Spacecraft processing facility monitoring system (16 IP cameras, 48 TB archive, oxygen/propellant/temperature sensors, 18-month delivery). Customizable.
Technical specifications
- Purpose
- Video monitoring and parameter recording for spacecraft processing operations
- Year of release
- 2014
- Guaranteed service life, years
- 5
- Estimated production/delivery time
- 18 months
- Customization
- Can be adapted to customer requirements
- AC voltage
- 380/220 V, 50 Hz
- IP cameras
- 16 simultaneous, 3 MPix (1920×1080), 25/30 fps, H.264 (or MPEG-4)
- Operational archive, TB
- 48 (12 × HDD)
- Monitored parameters
- Oxygen content, propellant content, temperature, humidity
- Components
- Sensor set; fixed/rotating/portable cameras; data collection and processing; data archiving; operator workstation
- TRL
- 9
About
The Technical Condition Monitoring System provides wide-angle and close-up video monitoring and recording of spacecraft processing operations, along with collection, analysis, and recording of oxygen content, propellant content, temperature, and humidity parameters. It alerts personnel via sound and light alarms when parameters are exceeded, and manages a monitoring database. The system simultaneously operates 16 IP cameras at 1920×1080 / 25-30 fps H.264, with a 48 TB operational archive (12 HDD). AC power: 380/220 V, 50 Hz. Released in 2014 with 5-year service life and 18-month delivery time. Adaptable.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.
