
Key highlights
- Deployable elements: 2
- Deployment Configuration: 135°/90°
- Front side power: 15 W
- Backstring option: +7.5W
- Body mounted option: +7.5W
- Total Power: 30 W
- Peak platform power: 37.5 W
- OC Voltage: 15.6 V
- Suggested for: 3U/6U
- Deployment System: Dual redundant
- Integrated thermal sensor and photodiode.
- Qualified under NASA GEVS and ESA ECSS standards, fully CubeSat-compatible.
Applications
- Power generation for 3U/6U CubeSat missions in LEO and GEO.
- Supporting payloads with higher energy requirements, such as advanced sensors, telecom systems, or scientific instruments.
- CubeSat missions requiring reliable deployable solar arrays to maximize energy production.
Key features
- Redundant HDRM
- Redundant Deployment Feedback
- Integrated photodiodes
- Integrated Thermal sensors
Customization
- Customizable PV strings connection
- Customizable cut-outs and fixing holes
- Customizable cut-outs for radiators/sensors
- Customizable deployment layout
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Last updated: 2025-12-15

Technical specs
form factor
3U
voltage
15.6 V
bol-efficiency
>30%
peak power
15 to 30 W
deployment angle
90 to 135 deg
redundancy
Dual Redundant
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