More power for your mission

3U Deployable Solar Array

Fully qualified deployable Solar Array

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

Fully qualified deployable Solar Array

29.5%triple junction
solar cells
8.4 Win LEO
per side

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



science and research iconScience and Research
Earth Observation iconEarth Observation
IoT and communications iconIoT and Communications
In-orbit demonstration and verification iconIOD/IOV

Integrated sun sensors and gyroscope option - backbone for ADCS

3u-deployable-xy-mtq-rbf-cubesat-solar-panel-endurosat magnetorquer and remove before flight pin


Power efficiency at EOL 29+%
Max Power Up to 8.4 W in LEO per side
Internal By-pass diode reverse bias protection
Solar cells thickness 150 μm ± 20 μm
Sensors Temperature and Sun, optional Gyroscope
MTQ Connector for external magnetorquer
RBF Available with Remove Before Flight pin
Mass 270 g (320 g with MTQ)
Customisation Multiple panels can be connected in series or parallel
Max Voltage 16.8 V (for 7 cells)
Max Current 504 mA
PCB Thickness 1.6 mm

Series or parallel connection based on client power system requirements

3u-deployable-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