HARDWARE / PRODUCTAdded 25 Aug 2026

D-SP3X-L-2W

NPC Spacemind
D-SP3X-L-2W

The D-SP3X-L-2W is a deployable solar panel system designed for CubeSat structures, featuring a 2 Wings Lateral Configuration and high-efficiency triple junction UTJ solar cells.

Typed specifications14 values

Discloses 4 of 12 fields engineers filter by in this category (category median 3).

Output power (BOL)
16–17.6 W
P Max · datasheet p.2
Form factor (as printed)
XY side
datasheet p.2
Deployable
yes
datasheet p.1
Power consumption
16–17.6 W
product page
Data interface
SPI
datasheet p.1
Fits satellite size
3U
compatibility 3U/6U · datasheet p.2 6U compatibility 3U/6U
Integrated devices
temperature sensor
datasheet p.2 coarse sun sensor optional sensor add-on: 4  |  gyroscope optional sensor add-on: IMU (3D Acc + 3D Gyro)  |  other optional sensor add-on: magnetic sensor (3 axis)
Connector
Power connectors: 2 x parallel
datasheet p.2
Satellite class
CubeSat
datasheet p.1
Integrated sensors (as printed)
Optional add-on: digital temperature sensor (SPI / I²C), NTC temperature sensor, 4 coarse sun sensors, IMU (3D Acc + 3D Gyro), magnetic sensor (3 axis)
datasheet p.2

Each value is typed with its unit and measurement condition and cites the datasheet page it was taken from. Nothing is guessed: a field that is absent here has not been published by the manufacturer. machine-extracted ✓ checked by NewSpace Market ✓ manufacturer confirmed by the manufacturer.

As published by the supplier5 lines, in the manufacturer's own wording
Configuration
2 Wings Lateral
Compatibility
3U/6U CubeSat structures
Solar Cells
High efficiency triple junction UTJ
Peak power
16 – 17.6 W
Power connectors
2 parallel picoblade

About

The D-SP3X-L-2W is a deployable solar panel specifically designed for the XY side of CubeSat structures, featuring a 2 Wings Lateral Configuration. It is compatible with both 3U and 6U CubeSat structures. This system utilizes high-efficiency triple junction UTJ solar cells, providing a peak power output ranging from 16 to 17.6 W. For power connectivity, it includes 2 parallel picoblade power connectors. The D-SP3X-L-2W also offers an option to add additional solar cells on the body fixed surface for increased power generation. Customization options are available to meet specific mission requirements. Further options include a digital temperature sensor with SPI / I2C communication, an NTC temperature sensor, 4 coarse sun sensors, an inertial module (3D Accelerometer + 3D Gyroscope), and a 3-axis magnetic sensor.

Documentation

Need the full ICD, test reports or a specific revision? Ask the supplier directly.

Source: www.npcspacemind.com ↗

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