Power in space

1.5U Solar Panel

Flight-proven 1.5U Solar Panels

this cubesat module is featured in NASA state of the art report
1.5u-xy-mtq-rbf-cubesat-solar-panel-endurosat-cropped

Flight-proven 1.5U Solar Panels

29.5%triple junction
solar cells
ADCSready
sensors
3.6 Win
LEO

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

1.5u-xy-mtq-rbf-cubesat-solar-panel-endurosat-efficiency

High radiation resilience

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

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Applications

science and research iconScience and Research
Education iconEducation
Technology demonstration iconTechnology Demonstration

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

1.5u-xy-mtq-rbf-cubesat-solar-panel-endurosat magnetorquer and remove before flight pin

Features

Power efficiency at EOL 29+%
Max Power Up to 3.6 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 65 g (79 g with MTQ)
Customisation Multiple panels can be connected in series or parallel
Max Voltage 4.8-7.2 V (for 3 cells)
Max Current 504 mA
PCB Thickness 1.6 mm

Series or parallel connection based on client power system requirements

1.5u-xy-mtq-rbf-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