Star Tracker LEO
- Purpose: Star based satellite attitude determination
- Year of release: 2019
- Guaranteed service life (years): 5
- Estimated production / delivery time (months): 6
- Flight qualification of the product: No
- Brief history of flight qualification: Prototype flight experience over 7 years
- Possibility to adapt the product to customer requirements: Yes
| Parameter | Value |
|---|---|
| Random error (1-sigma) across boresight at 22 Hz | 1,5 arcsec |
| Random error (1-sigma) boresight at 22 Hz | 10 arcsec |
| Random error (1-sigma) across boresight at 10 Hz | 1 arcsec |
| Random error (1-sigma) boresight at 10 Hz | 7 arcsec |
| Mass (including 30 grad baffle) | 0,5 kg |
| Dimensions (including 30 grad baffle) | 149 х100 х137 mm |
| Power consumption | 5 W |
| Sun exclusion angle | 30 grad |
| Power | 10…32 V |
| Temperature range | minus 40… plus 50 |
Autonomous Star Tracker
Remark
Designed for LEO up to 1200
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