Chiyu Solar Energy System
Hongqing Technology (鸿擎科技)
The Chiyu Solar Energy System is Hongqing Technology high-performance solar wing product line designed for LEO satellite platforms. It features a high deployment-to-storage ratio enabling compact stowage during launch and full solar array deployment on orbit, and a high power-to-weight ratio to maximize electrical output per kilogram of mass. Available in single-wing and dual-wing configurations, […]
Key figurescomparable across the catalogue
- Power
- 1,000 W
Normalised to common units so this product can be compared with others in its category. The supplier's own wording is below.
As published by the supplier
- Type
- Deployable solar wing / solar array
- Configurations
- Single-wing, dual-wing
- Power output range
- 1,000 W - 8,000 W
- Deployment-to-storage ratio
- High (optimized for compact launch stowage)
- Power-to-weight ratio
- High (optimized for LEO mass constraints)
- Target orbit
- Low Earth Orbit (LEO)
About
The Chiyu Solar Energy System is Hongqing Technology high-performance solar wing product line designed for LEO satellite platforms. It features a high deployment-to-storage ratio enabling compact stowage during launch and full solar array deployment on orbit, and a high power-to-weight ratio to maximize electrical output per kilogram of mass.
Available in single-wing and dual-wing configurations, the Chiyu system scales to meet diverse mission power requirements from small satellites to high-power constellation nodes. The power output range of 1,000 W to 8,000 W covers the full spectrum of commercial LEO satellite applications, from communication relay nodes to high-throughput broadband and remote sensing payloads.
The system is designed for mass production and high reliability, consistent with Hongqing Technology constellation deployment philosophy of low cost and rapid scalability.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.