SATJ30

SAT Wings

SolarPanels for Satellites
LEO MEO and GEO satellite long term and reliable electrical powersupply system is based on mass produced and can be customizedsolar cells in depending solar array configuration to fulfill differentmission requirements.The solution adopt upright lattice-matched structure of SATJ30solar cells,provide exceeds 30% electrical energy averageconversion.

  • Key features
    Orbit:LEO,MEO,GEO
  • Substrates& size can be customizedlong design life
    High conversion efficiencyaverage 30%Pass diode protection
  • Variety ofassembly

Technical Specifications
Design and MechanicalData
Substrate Material Ge
Base Material GalnP/GaAs/Ge
Size(mm) 40.0x80.0,60.0x120.0,67.0x138.0
Thickness(μm) 180±20
Average Weight(mg/cm2) ≤110
Service orbit LEO, MEO, GEO
Typical Performance Data
Fluence (e/cm²) BOL; 1E14; 5E14; 1E15
Efficiency nbare (%) 30; 28.8; 27; 25.8
Short Circuit Jsc(mA/cm²) 17.5; 17.4; 16.8 ;16.3
Open Circuit Voc(V) 2.75; 2.64; 2.58; 2.53
Current @ Max.Power Jm(mA/cm²) 16.6; 16.4; 16; 15.5
Voltage @ Max. Power Vm (V) 2.45; 2.38; 2.28; 2.25
AM0(1353W/m2,T=25°C))
Temperature Gradients
Short Circuit Jsc (μA/cm²/°C) 12
Open Circuit Voc (mV/°C) -5.6
Current @ Max. Power Jm (μA/cm²/°C) 9
Voltage @ Max. Power Vm (V/°C) -5.8
Temperature Coefficient(20°C~80°C)
Description
Substrate Ge
Solar cell structure GalnP2/GaAs/Ge
GaAs growth method MOCVD
Thickness 175μm,140μm
Size(mm) 39.8x60.4; 30.6x40.3; 40x80
Bypass diode Separate external; bypass diode; assembled at corner

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SAT Wings

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