Generating power for complex missions

6U Deployable Solar Array

Fully qualified deployable Solar Array

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

Fully qualified deployable Solar Array

29.5%triple junction
solar cells
19.2 Win LEO
per side

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


Industry-leading redundant burnwire mechanism with feedback configurable for X/Y or Z side deployment


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

High radiation resilience

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



Power efficiency at EOL 29+%
Max Power Up to 19.2 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 Integrated H-Bridge for control of external magnetorquer
RBF Available with Remove Before Flight pin
Mass 757 g
Customisation Multiple panels can be connected in series or parallel
Max Voltage 19.2V (8s2p), 9.6V (4s4p)
Max Current 1А (8s2p), 2A (4s4p)
PCB Thickness 1.6 mm

Integrated sun sensors and gyroscope option - backbone for ADCS

Series or parallel connections compatible with diverse power system requirements



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