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Space Solar Cells

Space Solar Cell Assembly

YIM offers a range of 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.The interconnectors are covered with silver or kovar, fixed by a sophisticated welding process and designed for LEO, MEO and GEO Missions.All used materials and components are space-qualified.Complies with standard ECSS E ST20-08C.

Characteristics is high output power,high strong anti-radiation capacity,wide application range. Our triple junction GaAs solar cells in missions like Yaogan-32, Moziji, Haiyang-2B, Beidou-42, Piaochong-5, Chang’e-4,wangtong-1, Beidou-3(M12), Gaofen-11(02), ZY-3(03),NH-1,TT-5 and so on, also hundrends of international satellites missions,  till now present very good performance. They are qualified for both Low Earth Orbit (LEO) and Geostationary Orbit (GEO) satellites according .

We also provide triple-junction GaAs solar array, solar arrays are consiste triple-junction GaAs solar cells or solar panels in a certain way of electrical assembly.


  • SC-3GA-1 Space Triple Junction Solar Cell Assembly
    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%
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  • SC-3GA-2 Space Triple Junction Solar Cell Assembly
    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%
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  • SC-3GA-3 Space Triple Junction GaAs Solar Cell Assembly 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%
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  • SC-3GA-4 Space Triple Junction GaAs Solar Cell Assembly Eff 32%.CIC
    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%
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  • Space Triple Junction Solar Cell Assembly 30%TJ80SCA
    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.
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  • FLEXIBLE GaAs SOLAR CELL
    Product Features:
    *High efficiency, thin thickness, adapted to the curved surface;
    *Weak light response is good, good quality consistency from every batch;
    *Low temperature coefficient and high power performance under high temperature.
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  • 30% Efficiency 1U solar panel (top/bottom)
    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).
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  • Cube Satellite, Star Chain Satellite Special Solar Panel
     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.
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  • 30% Efficiency Quickly Modular Solar Panels
        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
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Shanghai YIM of Space Power-sources specializes in supplying China Aerospace Group (CASC) space solar cell products. Shanghai YIM main tasks cover the design, supply, test and new product research of...

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