Key highlights
Space Inventor presents an advanced customizable microsatellite solution, crafted from modular Equipment for tailored missions. Our novel design reduces components, simplifying integration with easy 360° access.
The microsatellite platform is specifically engineered for the Falcon 9 quarter plate payload adapter and can utilize an 8-inch separation ring from ExoLaunch.
It is designed for reliability, and offers full flexibility to be adapted to specific customer needs. The platform features deployable solar panels with drive mechanism for optimal power generation further maximising the capabilities
Key features
Payload Mass Average: 10-70 kg
Payload Volume: Custom
Propulsion: Custom
Payload Power Peak Average: Up to 300 W
Reaction wheels: 4-8 x WHL 500/1000/5000
Payload Power Average: Up to 300 W
Battery Capacity: Up to 1200 Whr
Data Buses: Redundant CAN / Ethernet / SpaceWire
On-Board computer: Redundant Cortex-M7 /redundant Zync-7030
Bus provided redundant user data storage: Up to 64 GB
ADCS Pointing accuracy adv. option 1: Down to 5 arcsec
ADCS sensors: 6-12 Fine sun sensors, 1-2 star tracker, 2 gyros
Primary communications: S band 4 Mbps
High Speed links: 2 x S/X band 4 - 200 Mbps
Solar Peak power production: Up to 500 W
Available for GEO with reduced payload capacity and reduced link speed
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Last updated: 2025-04-09
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