CubeSat 6U Platform
IMT (Ingegneria Marketing Technologies)
IMT srl flexible 6U CubeSat platform with up to 115W solar power (with µSADA), <1deg pointing, X-band 50 Mbps downlink, 45-90 Wh battery, and 4U payload volume for 3-year LEO missions.
Key figurescomparable across the catalogue
- Payload capacity
- 6 kg
- Power
- 10 W
- Data rate
- 50 Mbps
- Design life
- 3 years
Normalised to common units so this product can be compared with others in its category. The supplier's own wording is below.
As published by the supplier
- Standard
- CubeSat 6U
- Solar power (body)
- 10 W peak
- Solar power (deployable)
- 50 W peak
- Solar power (with µSADA)
- 115 W peak
- Battery capacity
- 45 Wh or 90 Wh
- Pointing accuracy
- <1 deg (optional 0.1 deg)
- Frequency bands
- X / C / S / UHF / VHF
- X-band data rate
- Up to 50 Mbps
- Payload mass
- Up to 6 kg
- Payload volume
- Up to 4U
- Payload interfaces
- CAN bus, I2C (UART on request)
- Regulated buses
- 3.3 V, 5 V, 12 V
- Unregulated buses
- 32 V or 16 V raw
- Design lifetime
- 3 years LEO
About
The IMT srl CubeSat 6U Platform is a flexible satellite bus using COTS components to enable space missions developed within months at competitive cost. The platform supports body-mounted solar power at 10W peak, up to 50W with deployable panels, and 115W when paired with the IMT µSADA. Battery capacity is 45 Wh or 90 Wh. Pointing accuracy is better than 1 degree (optionally 0.1 degree). Supports multi-band communications including X-band at up to 50 Mbps, and payload interfaces via CAN bus and I2C. Payload mass up to 6 kg and payload volume up to 4U, with regulated power buses at 3.3V, 5V, 12V and unregulated raw buses at 32V or 16V. Operational lifetime is 3 years in LEO.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.