Core Components
星上智能算力系统
High-computing-power compact integrated electronic system
Joint research and development and application of core control chips for small satellites, achieving miniaturization and high computing power for satellite integrated electronic systems.
R&D cycle: 12 months
Joint research and development and application of smart supercomputers and their operating systems (based on the native HarmonyOS operating system) for small satellites, enabling satellite intelligence, onboard AI data recognition and processing, routing and forwarding, and data security.
R&D cycle: 12 months
High-performance supercomputer
Satellite intelligent control system
Space Laser Link System
- Bidirectional (transmit and receive) high-speed communication between satellites on the same or different orbits.
- Capable of asymmetric communication.
- Autonomous link establishment with high acquisition probability.
- Inter-satellite link distance:500km~5200km
- Access link distance：1500km~7500km
- Acquisition probability：≥95%
- Inter-satellite communication rate：1.25 / 2.5 / 5Gbps
Application：Various types of communication, navigation, and remote sensing satellites, integrated satellites, high and low orbit satellites, nanosatellites to small satellites (1Kg-1000Kg), agile satellites, etc.
Partner：CETC
Spatial Intelligent Power and Control System
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High specific impulse:2000-3000s
High Efficient:The thruster efficiency is
as high as50-80%
High thrust control accuracy:The resolution can reach 0.1%
High cost-effectiveness:The system with the same total impulse has a smaller mass.
Providing various optimal orbit-changing strategies
Principle： Orbit control system based on radio frequency plasma electric propulsion.
Application ：Satellites with wide-range orbital maneuvering and high velocity change, such as GEO satellites, LEO satellites, and deep space exploration spacecraft.
Source of technology：
Joint Laboratory for Satellite Intelligent Space Propulsion