Key highlights
The 3U Deployable Solar Array is a compact CubeSat deployable solar panel that lifts the power budget of 3U nanosatellites well beyond what body-mounted cells can provide. The single-deployable variant carries 14 triple-junction photovoltaic cells for a peak power of 16.8 W in LEO, while the double-deployable version stacks 21 cells to reach 25.2 W. Cell efficiency exceeds 30% at beginning of life and stays above 29% at end of life, and a burn-wire release mechanism actuates deployment. X/Y hinge mounting with selectable 90-degree or 135-degree deployment angles gives mission designers control over array orientation and satellite solar power capture.
Engineered for a five-year mission lifetime, the array runs from a single 5 V supply and shields its strings with internal bypass diodes against reverse bias. Up to three integrated photodiodes deliver coarse sun sensing, and an accessible remove-before-flight (RBF) inhibition mechanism keeps ground operations straightforward. Double-deployable wings can be connected in parallel for higher current, multiple arrays scale total power generation, and optional extras — an external magnetorquer connector, a low-power MCU, additional photodiodes, and a temperature sensor – adapt the panel to each spacecraft's ADCS and electrical power system. Every unit ships with a complete user manual and plugs directly into EnduroSat's CubeSat ecosystem.
Applications
- Primary power generation for 3U CubeSat missions in LEO
- Power-hungry 3U payloads (imaging, communications, IoT) exceeding body-mounted panel budgets
- University and commercial 3U nanosatellite programs needing a deployable solar array
- Missions tuning deployment geometry via 90 or 135 degree X/Y hinge angles
- Scalable satellite solar power using parallel-connected deployable wings
Key features
High-efficiency triple-junction cells:
14 cells (Single Deployable) or 21 cells (Double Deployable) with 30+% efficiency at BOL and 29+% at EOL.
Up to 25.2 W peak power in LEO:
16.8 W for the Single Deployable, 25.2 W for the Double Deployable configuration.
Selectable deployment angle:
X/Y hinge mounting options adjustable to 90 or 135 degrees.
Burn-wire release mechanism:
Reliable deployment actuation for the hinged wings.
Single 5 V operation:
Only one 5 V power supply is needed for operation.
Reverse bias protection:
Internal bypass diodes protect the cell strings.
Integrated sun sensing:
Up to 3 photodiodes plus an accessible RBF inhibition mechanism.
Scalable power:
Supports parallel array connections for custom power needs.
Configurable options:
Connector for external magnetorquer, low-power MCU, up to 2 extra photodiodes, and a temperature sensor.
Five-year design life:
Designed for a 5-year mission lifetime with radiation-resistant cell assemblies.
Testing & qualification
Fully qualified under ESA Standard ECSS E ST20-08C for LEO and GEO orbit
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Last updated: 2026-06-04
Technical specs
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