Size: 30% Triple Junction Solar Cell（CIC）
Area: 1200mm2/Size: 40.0mm×30.0mm /Thickness: 155±20 um 
Weight:<125mg/cm2（with cover glass and bypass diode ） Typical Electrical Parameters (AM0, 135.3mW/cm2, 25℃)
Jsc=17.2mA/cm2,Voc=2.70V,Vm=2.36,Jm=16.4,Eff= 30%

Size: 30% Triple Junction Solar Cell（CIC）
Area: 2400mm2/Size: 60.0mm×40.0mm /Thickness: 155±20 um 
Weight:<80mg/cm2（with cover glass and bypass diode ）
Typical Electrical Parameters (AM0, 135.3mW/cm2, 25℃)
Jsc=17.2mA/cm2,Voc=2.70V,Vm=2.36,Jm=16.4,Eff= 30%

Size: 30% Triple Junction Solar Cell（CIC）
Area: 3015mm2/Size: 80.0mm×40.0mm /Thickness: 155±20 um 
Weight:<125mg/cm2（with cover glass and bypass diode ） Typical Electrical Parameters (AM0, 135.3mW/cm2, 25℃)
Jsc=17.2mA/cm2,Voc=2.70V,Vm=2.36,Jm=16.4,Eff= 30%

Size: 32% Triple Junction Solar Cell（CIC）
Area: 3015mm2/Size: 80.0mm×40.0mm /Thickness: 155±20 um 
Weight:<125mg/cm2（with cover glass and bypass diode ） Typical Electrical Parameters (AM0, 135.3mW/cm2, 25℃)
Jsc=19.1mA/cm2,Voc=2.70V,Vm=2.36,Jm=18.5,Eff= 32%

Technical Description 30%TJ80SCA
This cell type is an GaInP2/GaAs/Ge on Ge substrate triple junction solar cell assembly (efficiency class 30-32%). The solar cell assembly is equipped with an discrete Si bypass diode, interconnectors and cover glass.
Triple-junction GaAs Solar Array
Features
Triple-junction GaAs Solar Array is consiste Triple-junction GaAs Solar Array or solar panels in a certain way of electrical assembly.Characteristics is high output power,high strong anti-radiation capacity,wide application range.
Applications
LEO,MEO,GEO and explorations of the spacecraft
Flight experience
satellites of SJ series ,satellites of GY series.
Each product we will provide a rigorous test report.

Microsatellite
Cube satellites are representative of microsatellites and nanosatellites. The initial definition of a cube satellite was an external dimension of 10cm × 10cm × 10cm cube is also known as a cube satellite, consisting of multiple standard cube units (Units), such as 2U cube satellites, 3U cube satellites, 6U cube satellites, etc.
CubeSat Concept Definition
The interface between the solar panel and the satellite varies depending on the manufacturer, provided that the overall dimensions of the cube satellite comply with the specifications of the cube satellite. This product is compatible with ISIS (Innovative Solutions In Space) cubic satellite interfaces (Clyde and other standards can be customized).

 The RAMS (Rapid Assembling Modular Solar-panels) are solar panels that can be put together quickly. They have a thin carbon fiber-aluminum honeycomb board as their module structure, and a carbon fiber-aluminum honeycomb frame structure. With several modules and frames assembled, the panels can be put together quickly and used as either a spacecraft solar array plate or a development board. They can produce between 15W and 530W of power. These modular solar panels can be used with existing deployments and drive mechanisms, and can be up to 23mm thick.

    Rapidly modular solar panels (RAMS, Rapid Assembling Modular Solar-panle) with a thin carbon fiber - aluminum honeycomb board as a module structure, combined with carbon fiber - aluminum honeycomb frame structure, through a number of modules and frame assembly, you can achieve solar panels Of the rapid assembly and integration, both as a spacecraft solar array plate can also be used as a development board, the output power range of 15W ~ 530W. Modular solar panels can accommodate existing deployments and drive mechanisms with a total thickness of up to 23mm

1.As a byproduct in the production of triple junction gallium arsenide solar cells, the efficiency is comparable to that of model solar cells, and the cost is much lower than that of model solar cells. The advantages of heterotypic solar cells are also reflected in flexible layout and the ability to output various bus voltages on small modules.
2: There are two specifications: triangular and trapezoidal. The packaging of triangular solar cells can only use commercial SMT, while trapezoidal solar cells can use SMT or universal resistance welding technology for space solar cells.