module is featured in NASA state of the art report

29.5% efficiency space-grade solar cells

Dual burnwire deployment mechanism

Fully qualified under ESA Standard for LEO and GEO orbit

Series or parallel connection of multiple panels

High accuracy gyroscope, temperature and sun sensors

3U Single Deployable Solar Array


Power matters

Our 3U Deployable Solar Array utilizes fourteen highly efficient triple junction solar cells arranged into 1 fixed + 1 deployable panels. Fully compliant with the CubeSat standard, the deployable solar array doubles the energy generation capability of your satellite. Radiation and temperature resilience.

Included with this product

  • 5 hours of engineering support
  • Packed in a custom box
  • Full warranty
  • Technical information (Datasheet)

Technical Specifications

  • 1 Fixed + 1 Deployable 3U Solar Panels
  • Hinge: Short side, 90 degrees
  • Dual burnwire deployment mechanism
  • 14 Triple Junction Solar Cells InGaP/GaAs/Ge for Space Applications
  • Efficiency: 29.5 %
  • Internal By-pass diode for reverse bias protection
  • Fully qualified under ESA Standard ECSS E ST20-08C for LEO and GEO orbit
  • Solar cells thickness 150 μm ± 20 μm
  • Very low solar cell mass (81-89 mg/cm2)
  • High Radiation Resistance
  • Cover glass
  • Gyroscope (Optional)
  • Temperature Sensor (Accuracy: ±1.5°C from -25°C to 85°C (max), ±2.0°C from -55°C to 125°C (max)
  • Sun Sensor
  • Multiple arrays can be connected in series or parallel
  • Plated, countersink mounting holes with ground connection
  • Connector for external magnetorquer
  • Optimal Voltage – 16.31 V
  • Optimal Current – 1 A
  • Stowed configuration thickness: 6.2 mm
  • Total weight: < 300 g
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