Cubesat 3U Platform
Our platform meets a wide range of mission typologies:
Science, Earth observation, Technology demonstration.
About
Thanks to the IMT know how the mechanical and electrical architecture can support a very wide range of LEO orbit altitudes and inclinations. Redundant Architecture and Radiation Mitigation by Design can increase the Satellite Life-Time up to 5 years.
Performances
Dimensions | CubeSat 3U compliant |
---|---|
Mass | < 6 Kg |
Attitude Mode | Detumbling / Sun Pointing / Nadir Pointing |
Solar Panels | AzurSpace 3J Solar Cells (GaInP/GaAs/Ge) 30% + CoverGlass 100 CMX* Average Power: 4W (body mounted configuration) *Also available with Monocrystalline Si Cells |
Data BUS | I2C / CAN / SPI / UART |
Battery Pack | 43 Wh Li-ion Available configurations: 4S / 2S2P / 4P |
Payload Allowance | 1.5U / 3 W |
Power BUS | Reg. 3.3V (±1%) Max. 5A (latch-up protected) Reg. 5.0V (±1%) Max. 5A (latch-up protected) Unregulated |
Adapter | ISIPOD |
Attitude Stabilization | 3 axis stabilization |
Attitude knowledge accuracy | 5° |
Attitude control accuracy | 10° |
OS | Real Time OS - FreeRTOS |
Communications | Mod. J/B Uplink VHF (1200 bps AFSK) / Downlink UHF (9600 bps GMSK) Uplink UHF (1200 bps AFSK) / Downlink VHF (1200 bps AFSK) AX.25 Protocol (Available Custom Protocol) Transmission Power: Max. 2W Beacon: UHF (20 WPM @ 500 mW Transmission Power: Max. 2W |
Radiation | > 15 lRad (Si) SEU mitigation by design / SEL protection |
Random Vibration | 10 Grms (all axis) |
Data Storage | 64 MB for housekeeping data) 8 GB for payload data |
Life Time | < 5 years |