Our Dual-Axis Micro Analog Solar Sensor provides precise solar vector data crucial for optimizing reaction wheel usage. By accurately tracking the sun's position, the sensor allows for efficient solar panel pointing, maximizing power generation. This reduces the frequency and duration of battery discharge/recharge cycles, thus minimizing the load on reaction wheels needed for attitude correction due to power fluctuations. Optimized power management extends the lifespan of both the battery and the reaction wheels, leading to increased mission duration.

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.