HARDWARE / PRODUCTAdded 19 Aug 2026

Solis & Solis+ Spacecraft Solar Arrays

Dhruva Space
Solis & Solis+ Spacecraft Solar Arrays

Solis and Solis+ are Spacecraft Solar Arrays developed by Dhruva Space, optimised for reliability in Space, supporting satellites and spacecraft of various sizes with power capacities ranging from a few kWs to larger classes.

Typed specifications89 values

Discloses 7 of 12 fields engineers filter by in this category (category median 3).

Output power (BOL)
9.6 W
12Z · datasheet p.2 24 W 16X/Y  |  8.4 W 3X/Y  |  2.4 W 3Z  |  16.8 W 6X  +7
Cell efficiency
30 %
max · datasheet p.1 30 % max · up to 30%
Form factor (as printed)
off-the-shelf arrays 3Z, 3X/Y, 6Z, 6X, 12Z, 16X/Y for CubeSats 0.5U to 16U; custom arrays
datasheet p.3 12U, 16U 12Z  |  16U 16X/Y  |  3U, 6U 3X/Y  |  1U, 2U, 3U 3Z  +2
Deployable
yes
datasheet p.1 yes deployables with flight-proven hinges and HDRM (option)
Power consumption
2.4 W
product page 8.4 W  |  4.8 W  |  16.8 W  |  9.6 W  +1
TRL
9
datasheet p.2
Fits satellite size
0.5U
datasheet p.2 12U 12Z  |  16U 16X/Y  |  3U 3X/Y  |  1U 3Z  +19
Cell type
triple-junction GaAs
datasheet p.2
Integrated devices
temperature sensor
custom option · datasheet p.2 RBF connector custom option: access to RBF circuits  |  magnetorquer coil custom option: integrated magnetorquers  |  bypass diodes in CICs  |  other sun sensors (custom option)
Flight heritage
Solis Solar Arrays have flown on Dhruva Space's own satellites
datasheet p.2
Satellite class
CubeSat
datasheet p.2 CubeSat  |  CubeSat  |  CubeSat  |  CubeSat  +8
Substrate
FR4 PCB
FR4 substrate fabrication; CICs bonded to FRP (Fibre-Reinforc… · datasheet p.5
End-of-life power
2.4 W
datasheet p.2 9.6 W  |  24 W  |  2.4 W  |  2.4 W  +6
Deployment mechanism (as printed)
Deployables with flight-proven Hinges and Hold-Down and Release Mechanisms
datasheet p.1
Integrated sensors (as printed)
custom options: sun sensors, temperature sensors, integrated magnetorquers
datasheet p.2
Bypass diodes
per cell
CICs with integrated bypass diode · 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 supplier11 lines, in the manufacturer's own wording
Compatibility (Solis)
0.5U, 1U, 3U, 6U, 12U, 16U CubeSat platforms
Power (Solis 1U)
2.4 W
Power (Solis 3U)
8.4 W
Power (Solis 6U)
4.8 W
Power (Solis 12U)
16.8 W
Power (Solis 16U)
9.6 W
Power (Solis 16U) (2)
24.0 W
Power (Solis+)
few kWs
Cell efficiency (Solis+)
up to 30%
Cell type (Solis+)
Triple-junction GaAs CICs
Substrate (Solis+)
CFRP Honeycomb Sandwich

About

Solis Spacecraft Solar Arrays are designed to operate in the demanding conditions of Space, providing a reliable source of electrical power for various CubeSat platforms, including 0.5U, 1U, 3U, 6U, 12U, and 16U configurations. They feature mission-specific custom designs, deployables, and are LEO-optimised with faster turnaround times. Solis+ Spacecraft Solar Arrays operate in the demanding conditions of Space, offering power capacities in the order of a few kWs suitable for larger classes of satellites and spacecraft. Both Solis and Solis+ can be custom-designed by Dhruva Space’s team of design and engineering experts to meet specific mission requirements such as mass, power, longevity, and orbital parameters. Solis+ arrays boast high-efficient Triple-junction (up to 30%) GaAs Coverglass interconnected Cells (CICs), CFRP Honeycomb Sandwich substrate with local reinforcements, flight-proven hinges, and flight-proven, low-shock, and redundant Hold-Down and Release Mechanisms. They also support SADA (Solar Array Drive Assemblies) and BAM (Beta Angle Mechanism).

Documentation

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

Source: www.dhruvaspace.com ↗

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