 Technical facts


 | SSETI Express
| | 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 |
| Last update: 5 September 2005

 |  |  Related links

| | | SSETI Association Homepage (http://www.sseti.net) |  | | | SSETI Express Mission student site (http://sseti.gte.tuwien.ac.at/WSW4/MOPWS/index.php) |  | | | SSETI Radio Amateur Connection (http://sseti.gte.tuwien.ac.at/WSW4/MOPWS/ham.php) |  |

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