The Ultra-Compact Star Sensor plays a crucial role in optimizing satellite propulsion by providing highly accurate attitude determination. Precise attitude knowledge allows for more efficient and targeted thrust vectoring during orbit maintenance maneuvers or larger orbital changes. This reduces propellant consumption, extending mission lifespan or enabling more aggressive orbital adjustments. Our sensor's accuracy minimizes wasted thrust and ensures the propulsion system operates with maximum efficiency, particularly important for missions with limited propellant resources.

This system is compatible with microsatellites, nanosatellites, CubeSats, and larger spacecraft platforms. It features modular design with standard interfaces for easy integration into various mission architectures and supports both commercial and scientific applications.

The system provides advanced functionality with reduced size, weight, and power consumption. It offers improved reliability through redundancy, radiation tolerance, and proven space-qualified components with extensive flight heritage.

Key specifications include low power consumption, wide operating temperature range, high radiation tolerance (TID >100 krad), compact form factor, and long operational lifetime (>10 years). The system meets all relevant space qualification standards.

We provide comprehensive integration support including detailed interface specifications, test procedures, and simulation tools. All systems undergo thorough environmental testing, functional verification, and compatibility validation before delivery.