For commercial satellites and launch vehicles, Navcore uses its self-developed MEMS tactical-grade chip (bias <1°/h) as the core, with radiation-hardened design and vacuum adaptability optimization. This achieves order-of-magnitude reductions in size and power consumption compared to traditional fiber-optic gyroscopes.
The solution adopts multi-IMU redundancy + star sensor + GNSS integrated navigation, enabling rapid attitude establishment after satellite-vehicle separation and continuous tactical-grade attitude and orbit control data output in orbit.
- Cost: only 20%–30% of traditional solutions
- Delivery lead time: 4–8 weeks
- Fully independent and controllable supply chain