ISIS CubeSat solar panels

Flight heritage since 2013

ISIS CubeSat solar panels

€2500 - €8450

ISIS provides a range of high performance CubeSat compatible solar panels. The panels come in 1-6U size with sun and temperature sensors and other custom options available on request. Its space qualified cells are provided with extensive characterization and test reports. Thanks to its very thin and customisable design, it fits on all CubeSat structures and subsystems such as ISIS antenna system.

*price depends on the number of panels

Availability: 8 – 12 weeks

Sold By : ISISPACE SKU: N/A Category:
  • Features
  • Performance
  • Product properties
  • Testing
  • Available configuration
  • Documents
  • GaAs Triple-junction solar cells from AZUR Space
  • Body mounted on ISIS Aluminium or Carbon panels
  • Includes Coarse sun sensors and temperature sensors
  • Designed for LEO missions and requirements
  • Harnessing included
  • Manufactured according to space standards
    • ECSS-E-20-08
    • MIL-PRF-13830
  • Crack and flash tests provided with characterisation
  • Discounts for complete CubeSats solar panels sets
  • Applications
    • 1U/2U/3U CubeSats
    • 6U/12U/24U Nano satellites
  • Compatibility
  • Power Delivered:
    • 1U: 2.3 W
    • 2U: 4.6 W
    • 3U: 6.9 W
    • 6U: up to 17.2 W
  • Supply Voltage: 3V (5V and 8V on demand)
  • Cell Material: GaAs
  • Cell Efficiency: 30%
  • Mass (exact mass depends on configuration)
    • 1U: 50g
    • 2U: 100g
    • 3U: 150g
    • 6U: 300g
  • Panel Thickness:
    • Top/Bottom: 1.8 mm
    • Side Panel: 2.5 mm
  • Cover Glass: QioptiQ
  • Interconnector: Invar Silver plated
  • Interfaces:
    • Omnetics A25000 inline 8 pin connector
    • Raychem Spec44 cables (AWG26)
    • Harness included
  • Operating Temperature: -40 to +125°C
  • Radiation Tolerance: 2 years minimum in LEO
  • All panels are provided with tests reports regarding:
    • Continuity isolation between cells and substrate
    • Identification of solar cells cracks by thermo luminescence
    • I-V measurement by flasher test
Test QT AT
Mechanical Shock
Thermal Cycling
Thermal Vacuum
Total Ionizing Dose **
Continuity Isolation
Flasher Test
Solar cells Cracks

*QT is performed on the design qualification model
*AT is performed on the unit to be shipped
** Test performed on space qualified solar cells only

  • Top/Bottom 1U panels
  • On top of the ISIS AntS Antenna System
  • 1U/3U configuration
  • Deployable Panels
  • Dummy panels with sensors without cells