HARDWARE / PRODUCTAdded 25 Aug 2026

D-SP8X-L-2W

NPC Spacemind
D-SP8X-L-2W

The D-SP8X-L-2W is a deployable solar panel designed for the XY side of CubeSats, featuring a 2-wing lateral configuration and compatibility with 8U/16U CubeSat structures.

Typed specifications14 values

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

Output power (BOL)
46–50 W
P Max · datasheet p.3
Form factor (as printed)
XY side
datasheet p.3
Deployable
yes
datasheet p.1
Power consumption
46–50 W
product page
Data interface
SPI
datasheet p.1
Fits satellite size
8U
compatibility 8U/16U · datasheet p.3 16U compatibility 8U/16U
Integrated devices
temperature sensor
datasheet p.3 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: 4 x parallel
datasheet p.3
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.3

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 supplier1 lines, in the manufacturer's own wording
Peak power
46 - 50 W

About

The D-SP8X-L-2W is a deployable solar panel system from NPC Spacemind, specifically engineered for the XY side of CubeSats. It features a 2-wing lateral configuration, making it compatible with both 8U and 16U CubeSat structures. The system utilizes high-efficiency triple junction UTJ solar cells, providing a peak power output ranging from 46 to 50 W. For power connectivity, it includes 4 parallel picoblade power connectors. Customization options are available, including the ability to add additional solar cells on the body fixed surface. Further options include a digital temperature sensor (with SPI / I2C communication), an NTC temperature sensor, 4 coarse sun sensors, an inertial module (3D Acc + 3D Gyro), a magnetic sensor (3 axis), and alternative solar cell connection configurations.

Documentation

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

Source: www.npcspacemind.com ↗

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