The Monolithic Solar Sensor can provide precise solar vector information, which is crucial for optimizing the efficiency of electric propulsion (EP) systems on Starlink satellites. By accurately determining the sun's position relative to the satellite, the sensor enables precise adjustments to the solar panel orientation. This maximizes solar energy capture, ensuring sufficient power for the EP thrusters. Optimal power management leads to efficient orbit maintenance, collision avoidance maneuvers, and ultimately, extended satellite lifespan and reduced propellant consumption for Starlink.

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.