Technical facts
| Dimensions | 560 x 560 x 900 (maximum envelope) |
|---|---|
| Mass | 62 kg |
| Mass of payload | 24 kg |
| Expected lifetime | Minimum 2 months, extended mission until end of life |
| Attitude Determination System | Sun-sensors and magnetometer |
| Attitude Control System | Semi-passive magnetic stabilisation, plus a cold-gas payload |
| On-board Data Transfer | CAN. RS232 |
|
Telemetry -UHF -S-Band |
437.250 MHz, 9.6 kb/s, AX 25 2401.84 MHz, 38.4 kb/s, AX25 |
|
Power - Average -Peak |
Body mounted solar panels 12 W 20 W |
| Batteries | Li Ion, 90 Wh |
| Propulsion | 6l, 300 bar, Nitrogen cold gas |
| Camera | ~100m/pixel, 1280*1024 pixels, CMOS |
| Power Bes | 28V regulated |
| Thermal Control | Passive |
