Power in space

1U Solar Panel X/Y

Flight-proven 1U Solar Panels

this cubesat module has flight heritage
this cubesat module is featured in NASA state of the art report

Flight-proven 1U Solar Panels

29.5%triple junction
solar cells
2.4 Win

Triple Junction Solar Cells for Space Applications with efficiency higher than 29.5%


High radiation resilience

Cell efficiency higher than 29% even after 5 years in LEO



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Integrated sun sensors and gyroscope, optional magnetorquer - backbone for ADCS



Power efficiency at EOL 29+%
Max Power Up to 2.4 W in LEO
Internal By-pass diode reverse bias protection
Solar cells thickness 150 μm ± 20 μm
Sensors Temperature and Sun, optional Gyroscope
MTQ Available with integrated magnetorquer
RBF Available with Remove Before Flight pin
Mass 44 g (53 g with MTQ)
Customisation Multiple panels can be connected in series or parallel
Max Voltage 4.8 V (for 2 cells)
Max Current 504 mA
PCB Thickness 1.6 mm

Series or parallel connection based on client power system requirements

1u-xy-mtq-rbf-cubesat-solar-panel-endurosat parallel connection


user manual book icon Complete User Manual
included cables icon Power and data cables
customer support icon 1 hour engineering support
delivery cost icon Delivery cost
handling and administration costs icon Handling and administration costs