Mini4EO Satellite Platform
Deimos Space (Indra)
Multi-tasking small-satellite platform for Earth observation, capable of simultaneous imaging and downlink.
Technical specifications
- Wet mass
- 190 kg
- Dimensions
- 90 x 90 x 155 cm
- Service life
- 5+ years in LEO (extendable to 7 years)
- Maximum power
- 400 W (Sun Pointing mode)
- Battery capacity
- 1,555 Wh
- Agility
- ±45° in 15 seconds (roll/pitch, CMG-based)
- On-board processing
- AI-enabled imagery processing
About
Mini4EO is Indra Space’s (formerly Deimos Space) multi-tasking Earth-observation satellite platform, designed to perform simultaneous image capture and data downlink operations to maximise mission return. The bus offers a robust, modular construction that supports rapid in-orbit reprogramming and is compatible with multiple launch services, making it suitable for constellations as well as single-satellite missions. Mini4EO integrates agile pointing via control moment gyros (CMGs), giving it fast slew rates for tasking-intensive Earth observation, maritime surveillance and emergency-response missions. The platform is built and integrated at Indra Space’s ISO-7 clean-room satellite integration centre in Spain, drawing on more than two decades of small-satellite heritage from the original Deimos Space engineering team (Deimos-1, launched 2009, and subsequent missions). Mini4EO is offered as a complete, customisable mission solution including platform, ground segment integration and mission operations support.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.
