Overview
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
Properties
Overview
- Name
- M-1000 Smallsat Bus
- Supplier
- Momentus Space LLC
- Type
- SmallSat Bus
- Flight proven
- No