CubeSat ADCS Testing Facility
CubeSat 3U ADCS functional test bench (air bearing, sun simulator, magnetic field simulator, autonomous measurement system, 5000×3000×2500 mm, 250 kg) for orientation testing.
Technical specifications
- Purpose
- Functional testing of CubeSat 3U attitude determination and control system
- Year of release
- 2014
- Estimated production/delivery time
- 6 months
- Flight qualification
- No
- Customization
- No
- Test bench dimensions (min), mm
- 5000×3000×2500
- Test bench mass (min), kg
- 250
- Power supply, V
- 220
- Workstation processor, GHz
- 3
- RAM, GB
- ≥4
- GPU memory, GB
- ≥1
- Storage, GB
- ≥500
- Display resolution
- 1920×1080
- Balancing system
- Manual
- Components
- Air bearing (15 kg); CubeSat 3U platform; halogen sun simulator; magnetic field simulator; automated workstation; autonomous measurements system
- TRL
- 8
About
The CubeSat ADCS Testing Facility is designed for functional testing of CubeSat 3U attitude determination and control systems. It integrates an air bearing (15 kg), a CubeSat 3U satellite platform, a halogen sun simulator, a magnetic field simulator, an automated workstation, and an autonomous measurements system. Bench dimensions (min) 5000×3000×2500 mm, mass (min) 250 kg. Power 220 V. Workstation: 3 GHz processor, 4 GB RAM, 1 GB GPU, 500 GB HDD, 1920×1080 display. Balancing system is manual. Released 2014, 6-month delivery. Not flight qualified. Not customizable.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.
