Power in space

6U Solar Panel

Fully qualified Solar Panels

this cubesat module has flight heritage
this cubesat module is featured in NASA state of the art report
6u-x-y-cubesat-solar-panel-endurosat-cropped

Fully qualified Solar Panels

29.5%triple junction
solar cells
ADCSready
sensors
19.2 Win
LEO

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

6u-x-y-cubesat-solar-panel-endurosat-efficiency

High radiation resilience

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

6u-x-y-cubesat-solar-panel-endurosat-high-radiation-resilience

Applications

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

6u-x-y-cubesat-solar-panel-endurosat magnetorquer and remove before flight pin

Features

Power efficiency at EOL: 29+%
Max Power: Up to 19.2 W in LEO
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: 390 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

Multiple series and parallel connection options, covering diverse power system requirements

6u-x-y-cubesat-solar-panel-endurosat parallel connection

Included

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