Cell Engine

Sc33117 11S14P battery

LEO and small GEO satellites long term and reliable electrical power storage solution is based on mass produced space cells in depending battery configuration to fulfill different mission requirements.

Our solution adopt SP architecture (strings in parallel) of Sc33650/Sc33117 space cells,provide 50w to 2.5KW output to satellite platform.

This flight proven solution experienced more than 19 spacecrafts in orbit by the end of 2023.

Key features

  • Mass products flight proven
  • High energy density
  • Longdesign life (LEO 8-10 years, GEO 20 years)
  • High DoD (80% in GEO, 40%in LEO)
  • Cell stainless steel casing and hermetically sealed Compact and scalable configuration in s and p
  • Circuit breaker and venting at cell level
  • Thermalsensors, connector for power and telemetry

Technical Specifications
Operating coltage (V) 33-45
Output capacity(Wh) 700Wx0.6h
Balance management Independent balance,4.0V start and control
Initial capacity (Ah) ≥140
Size (mm) 595×615×150
Weight (kg) 43.2
Design life LEO 10 years
DOD(%) ≤40%
Operating temperature (°C) 10-35
Number of temperature telemetry 6

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