M-1000 Smallsat Bus

Balances design efficiency of Customization with production efficiency of commoditization
• Mission optimization over a broad range of applications
• High volume producibility for constellations from 1 to 100’s of spacecraft

Ready to Configure to Order each mission from a Standard set
of modules
• Pre-engineered for system level compatibility
• Commoditization/mass producibility at subsystem/module level
• Rapid turn around of a mission optimized solution (~1 year to 1st delivery)

The M-1000 is based on flight proven Vigoride technology and provides flexible mission configuration
• Rapidly configured for a wide range of mission requirements
• ~350 kg payload mass on rideshare or ~800 kg with dedicated launch
• Mission Configured Propulsion
• 1000W on orbit average power ~3 kw peak
• Dual redundant systems for assured reliability
• Scalable Mission Downlink Operationally Responsive Space

Schedule Targets
• Rapid build cycle
• Factory throughput: > 50/year initially further expansion within 24 months based on market demand

End-to-End Service Options
• Delivery in-orbit (i.e. launch service included)
• Mission Control Solution
• Long-Term Operations Service