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Advanced avionics and data processing

6U DEPLOYABLE SOLAR ARRAY

Generating power for advanced CubeSat missions
Cad file & datasheet
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Cad file & datasheet
29+%
TRIPLE JUNCTION SOLAR CELLS
ADCS
READY SENSORS
19.2 W
IN LEO PER SIDE

Space-qualified deployable Solar Array

FEATURES
Power Efficiency At EOL
29+%
Max Power
Up to 19.2 W in LEO per side per solar panel
Internal By-Pass Diode
reverse bias protection
Solar Cell Assembly (SCA) thickness
280-300 μm
Sensors
Temperature, Photodiode and Sun, optional Gyroscope
MTQ
Integrated H-Bridge for control of external magnetorquer
RBF
Available with Remove Before Flight pin
Mass
655-770 g (configuration dependent)
Flexibility
Multiple panels can be connected in series or parallel
Max Voltage
39.8V (16S2P), 19.9V (8S4P), 9,95V (4S8P)
Max Current
1A (16S2P), 2A (8S4PA), 4A (4S8P)
PCB Thickness
1.6 mm
6U Deployable Solar Array web render 1
Generating power for advanced CubeSat and SmallSat missions

Included

Complete User Manual
Power and data cables
1 hour engineering support
Delivery cost
Handling and administration costs
Space-qualified deployable Solar Array
6U Deployable Solar Array web 15
6U Deployable Solar Array web render 4

Triple Junction space-grade Solar Cells with efficiency higher than 29.5%

6U Deployable Solar Array web render 2 e1711026582826

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

6U Deployable Solar Array web render 3 e1711026609738

High radiation resilience

CELL EFFICIENCY REMAINS HIGHER THAN 29% FOR 5 YEARS IN LEO
6U Deployable Solar Array web render 5

Integrated sun sensors + gyroscope option

SERIES OR PARALLEL CONNECTIONS COVERING DIVERSE POWER SYSTEM REQUIREMENTS
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3000
MODULES IN ORBIT
120
DELIVERED SATELLITES
200
TB DATA DOWNLINKED
All our products undergo Space Qualification, involving stringent testing under extreme conditions to ensure robustness and high performance
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