SP1X
The SP1X is a solar panel designed for 1U CubeSat structures, featuring high-efficiency triple junction solar cells and integrated sensors for power generation and attitude determination.
Key figurescomparable across the catalogue
- Mass
- 0.04 kg
- Power
- 2.3 W
Normalised to common units so this product can be compared with others in its category. The supplier's own wording is below.
As published by the supplier
- Solar panel for
- XY side
- Compatible with
- 1U CubeSat structures
- Solar cells
- High efficiency triple junction UTJ
- Mass
- 40 g
- Peak power
- 2.3-2.5 W
- Current max power
- 500-520 mA
- Voltage max power
- 4.6-5 V
- Open circuit voltage
- 5.2-5.5 V
- Power connectors
- 2 parallel picoblade
- Sensors
- Digital temperature sensor, NTC, Coarse Sun sensor, IMU, Magnetic sensor
About
The SP1X is a solar panel specifically designed for the XY side of 1U CubeSat structures. It incorporates high-efficiency triple junction UTJ solar cells to maximize power generation in space environments. The panel is lightweight, with a mass of 40g, and can provide a peak power output of 2.3-2.5W. It features two parallel picoblade power connectors for electrical integration. Beyond power generation, the SP1X also includes several integrated sensors crucial for satellite operations: a digital temperature sensor, an NTC thermistor, a coarse sun sensor for attitude determination, an IMU (Inertial Measurement Unit), and a magnetic sensor. These integrated features make the SP1X a comprehensive solution for CubeSat power and basic attitude sensing needs.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.