Temperature significantly impacts solar cell efficiency. In space, without atmospheric convection, cells can experience extreme temperature variations. Higher temperatures reduce the band gap of GaAs, lowering the open-circuit voltage (Voc) and thus the overall power output. Our CICs are designed with temperature-compensating materials and processes to minimize these effects. Spacecraft thermal management systems are also crucial for maintaining optimal operating temperatures, maximizing efficiency and lifespan of the solar arrays. We provide detailed temperature coefficient data for accurate power prediction.

Designed for LEO, GEO, IGSO, and deep space exploration missions. Perfect for satellites, space stations, and long-duration spacecraft requiring high efficiency (>30%) and exceptional temperature tolerance (-175°C to 110°C) with proven 15+ year operational lifetime.

Superior efficiency (30-32%) outperforms standard solar cells by 40-50%, with exceptional radiation resistance maintaining 84-96% performance after high-dose exposure. Advanced encapsulation technology provides superior protection compared to conventional CIC designs, ensuring longer operational life.

Exceptional temperature coefficients ensure stable performance across extreme ranges (-175°C to 110°C). Advanced bypass diode protection (<1.0V forward voltage) and robust interconnectors (>1.6N pull strength) provide unmatched reliability. Superior thermal properties with optimal absorption and emissivity characteristics.

Standard CIC configuration with customizable dimensions (40×80mm to 67×138mm) enables integration into various solar array architectures. Compatible with both series and parallel string configurations for optimal power system design. Standardized electrical characteristics facilitate seamless integration with power conditioning units.