More power for your mission

3U Z 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
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