Solar Panels & Arrays

New Space company designing modular nanosatellite/CubeSat hardware: structures, solar panels, EPS, antennas, OBCs, and deployers/separation systems.

2NDSpace Srl

DROP-03 3U Deployable Solar panel

The DROP-03 is a deployable solar panel system designed for 3U and 6U CubeSats, offering a total power output of up to 22.5W with options for backstring and body-mounted cells.

Deployable elements	1
Deployment Configuration	135°/90°
Front side power	7.5W
Backstring option	+7.5W
Body mounted option	+7.5W

price on requestdatasheet

Aphelion Orbitals is a New Jersey-based launch vehicle company developing the Helios nanosatellite launch system for regular, scheduled orbital access at low cost.

Aphelion Orbitals

1U Solar Panel

The Aphelion Cubesat solar panels utilize flight-proven, high efficiency 30.5% triple junction solar cells and a reliable bonding technique.

Cell Efficiency	30.5% triple junction
Output Power	up to 150W
Output Voltage	up to 22V

price on requestdatasheet

US manufacturer of ultra-thin, lightweight CIGS thin-film flexible solar panels for spacecraft, UAVs, and extreme-environment applications, with on-orbit heritage.

Ascent Solar Technologies

CubeSat HDK Solar Array

The CubeSat Hardware Developer Kit packages Ascent Solar's flexible CIGS thin-film technology into body-mountable and folding solar arrays for 0.5U–6U CubeSat form factors, optimiz

Form Factors	0.5U, 1U, 3U, 6U
Array Configurations	Body-mountable and folding deployable
Bus Voltage	28 V
Technology	CIGS thin-film (Titan modules)
Specific Power	>2000 W/kg (bare modules)

price on request

Ascent Solar Technologies

EP-500V HDK Solar Array

The EP-500V HDK provides 500 V electric propulsion-optimized solar arrays in ESPA and ESPA Grande flatpack form factors, enabling direct high-voltage power delivery to Hall-effect

Output Voltage	500 V
Platform Compatibility	ESPA and ESPA Grande
Array Configuration	Flatpack folding deployable
Technology	CIGS thin-film (Titan modules)
Specific Power	>2000 W/kg (bare modules)

price on request

Ascent Solar Technologies

Smallsat HDK Solar Array

The Smallsat HDK delivers 28 V ESPA and ESPA Grande optimized flatpack folding solar arrays for small satellite missions, maximizing on-orbit power generation with Ascent's ultra-l

Platform Compatibility	ESPA and ESPA Grande
Array Configuration	Flatpack folding deployable
Bus Voltage	28 V
Technology	CIGS thin-film (Titan modules)
Specific Power	>2000 W/kg (bare modules)

price on request

Ascent Solar Technologies

Titan Bare Module

Ascent Solar's Titan is a monolithically integrated, flexible CIGS thin-film PV module optimized for space applications, achieving up to 2100 W/kg specific power at AM0.

Model	B-006-110-342
Technology	CIGS thin-film on flexible polyimide substrate
Titan Full – Pmax	16.5 W
Titan Full – Voc	34.2 V
Titan Full – Vmp	26.1 V

price on request

US small satellite manufacturer developing modular high-power solar array platforms for commercial and government GEO and MEO missions.

Astradyne

Advanced Solar Power Systems

Astradyne develops advanced, lightweight, and high-performance solar power systems for space and terrestrial applications, including solar arrays for next-generation space missions

Solar cell type	4-junction InGaP/GaAs/InGaAs
Efficiency	> 33%
Power output	10 – 25 kW
Configuration	Dual-wing deployable boom
Radiation tolerance	18-year GEO

price on request

Indian multi-sector technology company; Earth observation satellite development alongside electronics, composites, and agri-health services; satellite EO for food, agriculture, and healthcare.

AZUR SPACE designs and manufactures multi-junction solar cells and Coverglass Interconnected Cell assemblies for space and terrestrial applications.

AZUR SPACE

QJ 4G32-Advanced Space Solar Cell (4×8)

32% class quadruple-junction AlInGaP/AlInGaAs/InGaAs/Ge cell of 30.60 cm2 with 31.3% BOL efficiency and 3.3 g mass.

Part numbers	82921 (bare cell) / 82922 (assembly)
Base material	AlInGaP/AlInGaAs/InGaAs/Ge on Ge
Outer dimensions	40.08 x 80.08 mm (bare cell) / 40.26 x 80.26 mm (assembly)
Cell area	30.60 cm2 (glassed area 31.34 cm2)
Average weight	3.3 g bare cell (<= 109 mg/cm2) / 4.2 g assembly (<= 139 mg/cm2)

price on requestdatasheet

AZUR SPACE

QJ 4G32-Advanced Space Solar Cell (8×8)

32% class quadruple-junction cell of 60.35 cm2 with 31.1% BOL efficiency, 3415 mV open-circuit voltage and 6.5 g mass.

Part numbers	82883 (bare cell) / 82884 (assembly)
Base material	AlInGaP/AlInGaAs/InGaAs/Ge on Ge
Outer dimensions	80.00 x 80.00 mm (bare cell) / 80.15 x 80.15 mm (assembly)
Cell area	60.35 cm2 (glassed area 61.46 cm2)
Average weight	6.5 g bare cell (<= 107 mg/cm2) / 8.5 g assembly (<= 140 mg/cm2)

price on requestdatasheet

AZUR SPACE

QJ 4G32-Advanced Space Solar Cell (HP)

Large-format 32% class quadruple-junction cell of 77.44 cm2 in a 148 x 60.6 mm format, 30.8% BOL efficiency.

Part numbers	82902 (bare cell) / 82903 (assembly)
Base material	AlInGaP/AlInGaAs/InGaAs/Ge
Outer dimensions	148.06 x 60.56 mm (bare cell) / 148.26 x 60.76 mm (assembly)
Cell total area	77.44 cm2 (glassed area 78.62 cm2)
Average weight	10.4 g bare cell (<= 134 mg/cm2) / 13.6 g assembly (<= 175 mg/cm2)

price on requestdatasheet

AZUR SPACE

TJ 3G30-Advanced Space Solar Cell (4×8)

30% class triple-junction InGaP/GaAs/Ge bare cell and CIC assembly, 30.18 cm2, 29.5% BOL efficiency, 2.6 g bare cell.

Part numbers	81441 (bare cell) / 81442 (assembly)
Base material	InGaP/GaAs/Ge on Ge
AR coating	TiO2/Al2O3
Outer dimensions	40.00 x 80.00 mm (bare cell) / 40.15 x 80.15 mm (assembly)
Cell area	30.18 cm2 (glassed area 31.13 cm2)

price on requestdatasheet

AZUR SPACE

TJ 3G30-Advanced Space Solar Cell (6×12)

30% class triple-junction bare cell and CIC assembly of 71.25 cm2, 150 um thick, 6.1 g bare cell.

Part numbers	82943 (bare cell) / 82926 (assembly)
Base material	InGaP/GaAs/Ge on Ge
AR coating	TiO2/Al2O3
Outer dimensions	60.5 x 124.3 mm (bare cell) / 60.7 x 124.5 mm (assembly)
Cell area	71.25 cm2 (glassed area 72.65 cm2)

price on requestdatasheet

AZUR SPACE

TJ 3G30-Advanced Space Solar Cell (8×8)

30% class triple-junction bare cell and CIC assembly of 60.35 cm2 with 29.3% BOL efficiency and 5.2 g bare cell mass.

Part numbers	81780 (bare cell) / 81752 (assembly)
Base material	InGaP/GaAs/Ge on Ge
Outer dimensions	80.00 x 80.00 mm (bare cell) / 80.15 x 80.15 mm (assembly)
Cell area	60.35 cm2 (glassed area 61.46 cm2)
Average weight	5.2 g bare cell (<= 86 mg/cm2) / 7.1 g assembly (<= 118 mg/cm2)

price on requestdatasheet

AZUR SPACE

TJ 3G30-Advanced Space Solar Cell (HP)

High-power 30% class triple-junction cell of 77.55 cm2 in a 145.9 x 60.7 mm format, 10.4 g bare cell.

Part numbers	82942 (bare cell) / 82924 (assembly)
Base material	InGaP/GaAs/Ge on Ge
Outer dimensions	145.90 x 60.69 mm (bare cell) / 146.10 x 60.89 mm (assembly)
Cell area	77.55 cm2 (glassed area 78.64 cm2)
Average weight	10.4 g bare cell (<= 134 mg/cm2) / 13.1 g assembly (<= 170 mg/cm2)

price on requestdatasheet

Developer of deployable solar arrays delivering scalable power for orbital data centers, space stations, and lunar operations.

Leading provider of small satellite buses, systems, and components for commercial, civil, and government space missions, a Raytheon (RTX) business.

Blue Canyon Technologies

Solar Arrays

Blue Canyon Technologies offers flight-proven, high-efficiency solar arrays for various satellite platforms, providing reliable power for onboard systems.

3U Solar Array Power	27 – 34 W
3U Array Voltage, VMP	14.9 VDC
6U/12U Solar Array Power	48 – 118 W
6U/12U Array Voltage, VMP	17 or 34.1 VDC
ESPA-Class Microsatellite Solar Array Power	222 – 444 W

price on requestdatasheet

CAVU Aerospace designs and manufactures spacecraft avionics, including radiation-tolerant onboard computers, thermal control units, frame grabbers, and flight-proven satellite cameras for various spac

CAVU Aerospace

30% Efficiency Triple Junction GaAs Solar Cell

A high-performance triple-junction GaAs solar cell with 30% efficiency at BOL, designed for demanding space applications including LEO, GEO, interplanetary spacecraft, CubeSats, an

Efficiency	30% at the beginning of life (BOL) under standard AM0 conditions
Technology	Triple Junction GaInP/InGaAs/Ge
Radiation Resistance	Retains significant efficiency after exposure to radiation doses up to 1×10¹⁵ e/cm²
Bypass Diode Integration	Built-in silicon bypass diode
Dimensions	80.15mm × 40.15mm

price on requestdatasheet

CAVU Aerospace

32% Efficiency Triple Junction GaAs Solar Cell

A premium, high-efficiency triple-junction GaAs solar cell designed for space missions, offering 32% efficiency at BOL and robust radiation tolerance for LEO and deep space applica

Efficiency at BOL	32%
Open Circuit Voltage (Voc)	2.666 V
Maximum Power (Pmax)	1.331 W
Efficiency (AM0 spectrum, 25°C)	32.63%
Radiation Tolerance	Maintains efficiency after exposure to high radiation levels

price on requestdatasheet

CAVU Aerospace

Space Solar Panel

The Space Solar Panel is a customizable power generation solution for satellites, offering bespoke designs based on mission requirements for voltage, power, mass, dimensions, and d

MATERIAL EM	FR4 PCB, Aluminium PCB
MATERIAL QM	Aluminium honeycomb wings, HDRM, SADA
MATERIAL FM	Carbon Honeycomb (2.6 kg/m2) or Carbon Honeycomb (1.8 kg/m2), HDRM, SADA

price on requestdatasheet

Comat is a French aerospace equipment manufacturer, part of the Hemeria group, designing flight hardware and mechanisms for small satellites, telecommunications/observation payloads, and space exploration missions.

Comat

SADM-200

The SADM-200 is a compact Solar Array Drive Mechanism (SADM) developed by COMAT for small satellites, capable of handling up to 200W per solar array wing with integrated slip rings

Power (qualified)	200W at 28V
Power (transfer capability)	400W at 50V
Torque	350 mNm
Pointing Accuracy	3°
Communication Interface	RS 485

price on requestdatasheet

CTD develops state-of-the-art composites for extreme conditions and demanding applications in aerospace, high performance magnets, cryogenic systems, marine, automotive, and industrial sectors.

CTD (Composite Technology Development)

CLASP Composite Lightweight Array with Shape-memory Polymer

Deployable composite solar array with shape-memory polymer hinges: over 250 W/kg specific power and 110 kW/m3 packaging efficiency, CubeSat dispenser compatible.

Specific power	Exceeds 250 W/kg
Packaging efficiency	110 kW/m3
Deployment	Shape-memory polymer based composite architecture
Dispenser compatibility	CubeSat dispenser compatible
PV cells	Accommodates all PV cells; fit for purpose and mission budget

price on requestdatasheet

Indian CubeSat developer offering flight-ready 1U–6U satellite structures, subsystem components, environmental testing services, launch integration, and STEM education programs from Ahmedabad.

CubeSat Aerospace

1U Solar Panels

The 1U Solar Panels from CubeSat Aerospace are high-efficiency power generation modules designed for small satellites, integrating solar cells, magnetic torquers, and sun sensors i

Panel Type	Custom PCB-based solar panel
Solar Cells	Mono-crystalline high-efficiency cells
Output Voltage	11.5 V (regulated via avionics board)
Power Output	Up to 1 W per panel (depending on illumination)
Mounting Faces	X+, X–, Y+, Y–, Z+, Z– (6 panels for full 1U coverage)

price on request

German manufacturer of space deployables using patented Shape Memory and Origami technologies — release actuators, solar arrays, and antenna deployables for CubeSats and microsatellites.

Dcubed

Body-Mounted Solar Array

Fixed body-mounted solar panels for CubeSats and smallsats, with triple-junction GaAs cells pre-integrated onto structural panels for immediate spacecraft integration.

price on request

Dcubed

Flexible Blanket Solar Array

Dcubed's Flexible Blanket Solar Array is a compact, lightweight, and durable solar array designed for spacecraft, offering high power generation for a given mass and volume.

EOL Power

up to 2kW

price on request

Dcubed

Origami Solar Array

The Dcubed PowerCube is a deployable 100W Origami Solar Array stowed within a 1U form factor, enabling high-power space missions with minimal stowed volume.

Short Delivery Time	12 months
EOL power	100 W (5 years lifetime)
Stowed volume	100x100x100 mm (1U)
Deployed volume	110x110x190 mm
Mass	1.2 Kg

price on request

Deployable Space Systems (DSS), now part of Redwire, develops and produces the ROSA (Roll-Out Solar Array) — the deployable solar wing powering ISS upgrades, DART, and the Gateway PPE.

Deployable Space Systems (DSS) — now Redwire

ELSA

ELSA (Extensible Low-Profile Solar Array) is an innovative power solution designed to minimize solar array stowed volume and mass, offering 50% more power by volume than traditiona

PAYLOAD SIZE (STOWED)	Configurable per mission requirements
POWER (BOL)	500W to 5kW
SOLAR CELL TECHNOLOGY	Cell Agnostic: ELSA can support III-V and Silicon technologies
STOWED FIRST MODE	>40Hz standard
DEPLOYED FIRST MODE	>.25Hz standard

price on request

Deployable Space Systems (DSS) — now Redwire

ROSA Roll-Out Solar Array (Redwire / DSS)

Blanket-type roll-stow solar array from Redwire (DSS heritage) — flight proven on ISS iROSA (boosted power by 30%), DART, and in development for Lunar Gateway PPE.

Array type	Roll-stowable blanket photovoltaic
Flight heritage	ISS iROSA (6 wings), DART mission
ISS power increase	~30% (160 kW → ~215 kW total station power)
In development	Lunar Gateway Power & Propulsion Element (PPE), 2 wings
Stow configuration	Compact cylindrical cannister

price on request

DHV Technology is a Spanish space technology company designing and manufacturing solar panels, electrical power systems, MLI blankets, and solar array drive assemblies for CubeSats and small satellites. Based in Málaga since 2013.

DHV Technology

CubeSat Solar panel DHV-CS-10

Solar panels have been tested in qualified laboratories for space applications, as well as solar cells are fully qualified. Different mechanical and electrical designs can be…

Manufacturer	DHV Technology
Lead time	4 – 5 weeks

€1 450

DHV Technology

Solar Panels for Small Satellites

Custom deployable solar array panels for small satellites above 12U, up to 100 kg class, with triple-junction cells and structural integration support.

price on request

Software-flexible CubeSat platforms (1U–16U+), shared-satellite hosted-payload service.

EnduroSat

3U Solar Panel

Body-mounted 3U solar panel with space-grade triple junction cells delivering over 30% efficiency. Generates up to 8.4 W in LEO while maintaining performance throughout the satelli

Power Efficiency (BOL)	30+
Solar Cells	7
Max Power in LEO	8.4
Max Voltage	17.5
Max Current	512

price on request

EnduroSat

6U Deployable Solar Array

A deployable solar panel array for 6U CubeSats that unfolds after launch to increase illuminated solar cell area and boost power generation beyond what body-mounted panels can prov

Power Efficiency @ EOL

29+%

price on request

Ecuadorian civilian space agency and manufacturer of high-energy-density batteries, deployable solar arrays and CubeSat platforms.

EXA (Ecuadorian Space Agency)

EXA DMSA – Deployable Multifunction Solar Array

The EXA D MSA: Deployable Multifunction Solar Array with embedded antennas, magnetorquers and sensors is the upgraded version of the latest DSA 1/A, it is our entry-level product…

Manufacturer

EXA

price on request

Space technology startup developing flexible electronics and energy solutions for satellite and space applications.

Flexell

Flexible High-Efficiency Space Solar Arrays

Flexell's rollable and foldable ultra-high-power-density solar arrays using flexible thin-film photovoltaics for compact satellite power generation.

Technology	Flexible thin-film photovoltaics (CIGS or OPV) on polymer substrates
Deployment	Roll-out or fold-out (very compact stowed volume)
Specific Power	4–8× higher W/kg than rigid silicon panels
Efficiency	18–25% (thin-film multi-junction)
Applications	Smallsat power, HAPS aircraft, CubeSat arrays

price on request

Flexell

Nano-Thin Flexible Solar Module

Ultra-light, ultra-flexible wafer-less solar cells using ~1% of the silicon and 99% less energy than conventional production — ~95% lower carbon footprint.

Silicon use	~1% of conventional
Energy use	~99% less than conventional
Carbon footprint	~95% less than conventional

price on request

Glavkosmos coordinates international human spaceflight projects, facilitates satellite launches, develops and supplies rocket components, and provides equipment for space crews.

Glavkosmos

GaAs Solar Panel with Coils (end edge)

A GaAs solar panel designed for CubeSats, featuring built-in electromagnetic coils for stabilization and a super-diode protection circuit.

Year of release	2017
Guaranteed service life (years)	1
Estimated production / delivery time (months)	5
Flight qualification of the product	Yes
Brief history of flight qualification	In the composition of the satellites SiriusSat-1.2 (launched on 15.08.18.)

price on request

Glavkosmos

GaAs Solar Panel with Coils (side)

Flight-proven GaAs side solar panel for CubeSats with built-in electromagnetic coil for attitude stabilization, 28% efficiency.

Purpose	Electrical power source for CubeSat satellites with built-in electromagnetic coil for atti
Year of release	2017
Guaranteed service life	1 year
Estimated production/delivery time	5 months
Flight heritage	SiriusSat-1/2, launched 15 August 2018

price on request

Glavkosmos

Nanosatellite Solar Panel

The Nanosatellite Solar Panel is a solar cell board designed to generate electrical power for nanosatellites by converting light energy.

Purpose	Solar cell board designed to provide power for nanosatellite by converting light energy in
Year of release	2016
Guaranteed service life (years)	1 year
Estimated production / delivery time (months)	6
Flight qualification of the product	No

price on request

Glavkosmos

Si Solar panel with Coils (end edge)

A silicon solar panel for satellites, featuring built-in electromagnetic coils for stabilization and a robust mechanical design. It provides electrical power and can assist with sp

Year of release	2017
Guaranteed service life (years)	1
Estimated production / delivery time (months)	2
Flight qualification of the product	No
Possibility to adapt the product to customer requirements	No

price on request

Glavkosmos

Si Solar Panel with Coils (side)

A side-mounted silicon solar panel for CubeSats that serves as the electrical power source and includes a built-in electromagnetic coil usable for orientation and stabilization.

Year of release	2017
Guaranteed service life (years)	1
Estimated production / delivery time (months)	2
Flight qualification of the product	Yes
Brief history of flight qualification	In the composition of the satellites SiriusSat-1.2 (launched on 15.08.18.)

price on request

Glavkosmos

Solar Array Drive Mechanism. Type 4

An electromechanical solar array drive mechanism that continuously rotates satellite solar array wings at a controlled rate while transmitting electrical power and telemetry/contro

Output shaft rotation rate, deg/min	0-16
Angle measurement error, not exceeding, °	2.5
Total current of power current-collecting devices, A	90
Number of power supply circuits, units	18
Overall dimensions, mm	156 kh 260 kh 223

price on request

Glavkosmos

Solar Array Drive Mechanism. Type 6

The Type 6 Solar Array Drive Mechanism (SADM) is an electromechanical device designed for continuous rotation of solar array wings, electrical power transmission, and output shaft

Year of release	2008
Guaranteed service life (years)	10
Estimated production / delivery time (months)	12
Flight qualification of the product	Yes
Possibility to adapt the product to customer requirements	Yes

price on request

Glavkosmos

Solar Array Mechanical Device

A deployable solar array mechanical device providing power supply to spacecraft systems, capable of generating up to 25 kW of power.

Year of release	2007
Guaranteed service life	15 years
Estimated production / delivery time	18 months
Brief history of flight qualification	Amos-5, Yamal-300K, Express-AT1, Express-AT2, Express-AM8, KazSat-3, Loutch-5V, Express-AM
Solar array wing area	10 to 44 m2

price on request

GTM Advanced Structures is an AS9100-certified Dutch manufacturer of flight-ready solar panels for spacecraft and satellite missions, with over 80 SmallSat and 200 CubeSat solar panels deployed on orbit.

GTM Advanced Structures

Solar Panel Substrate Manufacturing and Photovoltaic Assembly

GTM-AS offers comprehensive in-house manufacturing services for satellite solar panels, covering substrate production, photovoltaic assembly, and final testing.

Substrate Manufacturing Capabilities	Lay-up skins
Substrate Manufacturing Capabilities	Bonded assembly
Substrate Manufacturing Capabilities	Autoclave cure
Substrate Manufacturing Capabilities	Machining
Substrate Manufacturing Capabilities	Integration inserts and brackets

price on request

Beijing satellite constellation company partnered with Blue Arrow Aerospace; develops communications, remote sensing, and science satellites plus in-house Jinwu propulsion, Chiyu power, and Baize electronics subsystems.

Hongqing Technology (鸿擎科技)

Chiyu Solar Energy System

The Chiyu Solar Energy System is Hongqing Technology high-performance solar wing product line designed for LEO satellite platforms. It features a high deployment-to-storage ratio e

Type	Deployable solar wing / solar array
Configurations	Single-wing, dual-wing
Power Output Range	1,000 W - 8,000 W
Deployment-to-Storage Ratio	High (optimized for compact launch stowage)
Power-to-Weight Ratio	High (optimized for LEO mass constraints)

price on request

IMT designs and develops Nano/Micro-satellites and on-board units for commercial, scientific, and defense applications, and provides EEE parts engineering.

IMT (Ingegneria Marketing Technologies)

IMT µSADA Miniaturized Solar Array Drive Assembly

ESA-funded miniaturized SADA for 6U/12U CubeSats with 6 triple-junction solar panels, 118W BOL output, ±0.3deg pointing, 250g drive unit mass, and CAN bus interface.

Compatible platforms	ISIS/GomSpace 6U, 12U CubeSats
Solar panels	6x triple-junction InGaP/GaAs/Ge, 100µm coverglass
BOL wing power	118W at 25°C
Bus voltage	31-54V (typ. 42V)
Bus current	2.6-3.0A (typ. 2.8A)

price on request

Dual-use clean energy and ISRU technology company developing automated solar manufacturing and regolith-processing systems for Earth and space.

Maana Electric

Green Cells HJT Solar Cell

Eco-friendly heterojunction (HJT) solar cell manufactured via Chemical Vapor Deposition instead of Physical Vapor Deposition — 90% less energy and 40% lower material cost.

Cell technology	Heterojunction (HJT)
Manufacturing process	Chemical Vapor Deposition (CVD)
Energy savings	90% less than PVD process
Material cost savings	40% lower

price on request

Maana Electric

TerraBox Solar Panel Mini-Factory

Deployable containerized mini-factory automating local solar PV panel assembly anywhere in the world — 1 panel every 6 minutes, 35 MW/year capacity, operational within 5 days.

Production rate	1 panel every 6 minutes
Annual capacity	35 MW/year
Deployment time	5 days to full function
Operator training	1 day
Cost reduction	~1/5 cost of conventional panels

price on request

MMA Design manufactures deployable solutions for space and terrestrial missions, including de-orbit systems and solar arrays, and is headquartered in Broomfield, Colorado.

MMA Design

24U CubeSat Solar Array (Very High Power)

330 W deployable solar array wing for a 24U DoD CubeSat with a 9-panel active surface — believed to be the largest deployable solar array ever flown on a CubeSat.

Power output	330 W (single deployed wing)
Active panel count	9 panels
Target platform	24U CubeSat (DoD mission)
Distinction	Largest deployable CubeSat solar array flown (per MMA)

price on request

MMA Design

FlexArray Solar Array System

Low-cost, high-reliability deployable solar array using proprietary thin-film membrane substrate with next-generation silicon solar cells — TRL 6, cell-agnostic design for constell

Substrate	Thin-film membrane
Solar cells	Next-generation silicon (cell-agnostic)
TRL	6 (ground qualification — thermal, vibration)
Target platform	Smallsat / constellation class
Quality standard	AS9100 certified

price on request

MMA Design

HaWK High Watts per Kilogram Solar Arrays

Rigid-panel deployable solar arrays delivering 36 W to 330 W, flight-proven on defense, exploration, and commercial missions including NASA's MarCO interplanetary CubeSats.

Power output range	36 W to 330 W
Panel type	Rigid deployable panel
Flight heritage	NASA MarCO interplanetary mission, defense and commercial missions

price on request

MMA Design

Solar Array Drive Assembly (SADA)

A gimbal mechanism that rotates a satellite's solar array wings to track the Sun, increasing average and peak orbital power.

Actuation range	+/-180 degrees
Feed-through conductors	Up to 16 signal/power feed-through conductors per wing
Actuation speed	Up to 2.2 degrees per second (adjustable per mission requirements)
Variants	6.5mm thick gimbal; 9mm gimbal (supports higher powered arrays)
Radiation tolerance	Radiation tolerant and fully radiation hard versions available for extreme environments be

price on request

mPower Technology develops and manufactures DragonSCALES, ultra-light, flexible silicon solar cell arrays for space power applications, with over 20 years of flight heritage originating from Sandia National Laboratories research.

mPower Technology

DragonSCALES

DragonSCALES is an ultra-light, ultra-adaptable silicon solar cell solution developed at Sandia National Laboratories, designed for high-volume, automated manufacturing with lower

High Packing Factor	Unique cell sizes yield greater power efficiency
Mesh Configuration	Isolates faults and eliminates single point failures
Radiation Resistant/Annealing	Withstands exposure with minimal degradation
Mechanical Flexibility	Malleable and integrable with any surface/form
Pre-Wired Components	Reduces handling and systems integration rework

price on request

mPower Technology

DragonSCALES Silicon Solar Cell Technology

Ultralight, mesh-configured silicon solar cell technology for space power — 3-5x lower cost than GaAs, 15-20 year radiation-recovery lifetime, flight-proven with OneWeb and Lynk Gl

Cell technology	Patented silicon solar cell (not GaAs/III-V)
Cost vs. GaAs	3-5x lower cost
Radiation lifetime	15-20 years (with annealing/recovery)
Architecture	Mesh configuration — fault isolation, no single-point failure
Mechanical properties	Flexible, shade tolerant, pre-wired

price on request

Pre-integrated nanosatellite buses (3U–16U+ MP42), green chemical propulsion, mission integration.

NanoAvionics

SmallSat GaAs Deployable Solar Panels

High-power triple-junction GaAs deployable solar panels for MP42 and MP42H microsatellite platforms, up to 225 W per wing in triple configuration.

Solar cell type	Triple-junction GaInP/GaInAs/Ge
Efficiency (typ.)	Up to 29.5%
Power generation capacity in LEO (AM0)	36.85 mW/cm²
Operating temperature	-40 °C to +85 °C
Structure	Aluminium honeycomb and carbon fiber

price on request

Thai CubeSat subsystems manufacturer and satellite solutions provider.

NBSpace

1U Solar Panel

1U-format photovoltaic panel from NBSPACE, built with space-grade materials for lightweight, compact CubeSat power generation.

Product family	Photovoltaic Panel (1U/3U/6U)
Form factor	1U
Materials	Space-grade materials for durability and optimal power generation
Design	Lightweight, compact, easy satellite integration

price on request

NBSpace

3U Solar Panel

3U-format photovoltaic panel from NBSPACE, built with space-grade materials for lightweight, compact CubeSat power generation.

Product family	Photovoltaic Panel (1U/3U/6U)
Form factor	3U
Materials	Space-grade materials for durability and optimal power generation
Design	Lightweight, compact, easy satellite integration

price on request

NBSpace

6U Solar Panel

6U-format photovoltaic panel from NBSPACE, built with space-grade materials for lightweight, compact CubeSat power generation.

Product family	Photovoltaic Panel (1U/3U/6U)
Form factor	6U
Materials	Space-grade materials for durability and optimal power generation
Design	Lightweight, compact, easy satellite integration

price on request

NPC Spacemind designs and manufactures CubeSat separation systems, deployers, and subsystems, including deorbiting systems, for nanosatellites and CubeSats.

NPC Spacemind

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 determi

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

price on request

NPC Spacemind

SP1Z

The SP1Z is a solar panel designed for CubeSat structures (1U/2U/3U/4U) featuring high-efficiency triple junction UTJ solar cells and integrated sensors.

Solar panel for	Z side
Compatible with	1U/2U/3U/4U CubeSat structures
Solar cells	High efficiency triple junction UTJ
Mass	45 g
Peak Power	2.3-2.5 W

price on request

NPC Spacemind

SP2X

The SP2X is a solar panel designed for 2U CubeSat structures, featuring high-efficiency triple junction UTJ solar cells and integrated sensors for attitude determination and temper

Mass	87 g
Peak Power	4.6-5 W
Current Max Power	500-520 mA
Voltage Max Power	9.2-10 V
Open Circuit Voltage	10.4-11 V

price on request

NPC Spacemind

SP3X

The SP3X is a solar panel designed for 3U/6U CubeSat structures, featuring high-efficiency triple junction UTJ solar cells and integrated sensors.

Solar panel for	XY side
Compatible with	3U/6U CubeSat structures
Solar cells	High efficiency triple junction UTJ
Mass	137 g
Peak Power	8-8.8 W

price on request

NPC Spacemind

SP6X

The SP6X is a solar panel designed for 6U/12U CubeSat structures, featuring high-efficiency triple-junction UTJ solar cells and integrated sensors.

Mass	335 g
Peak Power	18.4-20 W
Current Max Power	1-1.04 A
Voltage Max Power	18.4-20 V
Open Circuit Voltage	20.8-22 V

price on request

NPC Spacemind

SP8X

The SP8X is a solar panel designed for 8U/16U CubeSat structures, featuring high-efficiency triple junction UTJ solar cells and integrated sensors for power generation and attitude

Solar panel for	XY side
Compatible with	8U/16U CubeSat structures
Solar cells	High efficiency triple junction UTJ
Mass	450 g
Peak Power	23-25 W

price on request

San Francisco-based manufacturer of flight-proven CubeSat kits, SUPERNOVA nanosatellite buses, and spacecraft power/electronics components, with over 150 kits delivered and dozens of successful space missions since 2003.

Pumpkin, Inc.

135W Dual Articulated Deployable Solar Array

A compact, deployable 135W solar array with two single-motor Solar Array Drive Assemblies (SADAs) driving independently steerable 67W triple-panel solar arrays, compatible with Pum

Mass of array and SADAs	~4360 g (31 W/kg)
Bounding volume (12U)	~198812 cm^3
Bounding dimensions	227.3 cm x 36.5 cm x 23.9 cm
CoG & MoI	Available on request
String configuration option 1	3x 7S3P per half

price on request

Pumpkin, Inc.

220W Deployable Clamshell Solar Array (DCSA)

A compact 7U-stowed deployable solar array that unfolds into a 24-panel, 192-cell array delivering up to 220W of power for a wide range of spacecraft architectures.

Mass	~5050g (44W/kg)
Bounding volume	~6970cm^3
Bounding dimensions	43.9cm x 13.6cm x 11.6cm
CoG & MoI	Available on request
Stowed volume	7U

price on requestdatasheet

Pumpkin, Inc.

CubeSat Kit Fixed Solar Panel: End Panel

A 0.031in/0.8mm thick fixed (non-deployable) end-panel solar panel for CubeSat Kit satellites, built using Pumpkin's flight-proven PMDSAS construction methods.

SKU	710-00764
Panel Thickness	0.031in / 0.8mm
Solar Cell Type	Triple-junction solar cells, ~28% to >32% AM0 efficiency over product lifetime
Panel Family	Pumpkin Modular Deployable Solar Array System (PMDSAS)
On-Orbit Track Record	Over 600 PMDSAS panels flown since 2008 with 100% on-orbit success rate, LEO through GTO

$2 500

Pumpkin, Inc.

CubeSat Kit Fixed Solar Panels

Fixed (non-deployable) side/body-mounted solar panels for CubeSat Kit satellites, available in 1U, 1.5U, 2U and 3U cell configurations, built using Pumpkin's flight-proven PMDSAS c

Panel Thickness	0.031in / 0.8mm
Solar Cell Type	Triple-junction solar cells, ~28% to >32% AM0 efficiency over product lifetime
Panel Family	Pumpkin Modular Deployable Solar Array System (PMDSAS)
On-Orbit Track Record	Over 600 PMDSAS panels flown since 2008 with 100% on-orbit success rate, LEO through GTO
Quality Testing	Vacuum bakeout and comprehensive irradiance test performed on every panel

$2 500 – $5 650

Pumpkin, Inc.

Custom PMDSAS Panel, Body-Mounted, per Cell

Custom body-mounted solar panels built with Pumpkin's Modular Deployable Solar Array System (PMDSAS) technology, priced per solar cell, with a 100% on-orbit success rate since 2008

Technology	Pumpkin Modular Deployable Solar Array System (PMDSAS)
Mounting type	Body-mounted
On-orbit heritage	600+ panels flown since 2008, 100% on-orbit success rate, LEO to GTO
Solar cell efficiency (historical)	~28% AM0 (early triple-junction cells)
Solar cell efficiency (current)	>32% AM0

$1 250datasheet

Pumpkin, Inc.

Custom PMDSAS Panel, Deployable, per Cell

Custom deployable solar panels built with Pumpkin's Modular Deployable Solar Array System (PMDSAS) technology, priced per solar cell, with a 100% on-orbit success rate since 2008.

Technology	Pumpkin Modular Deployable Solar Array System (PMDSAS)
Mounting type	Deployable
On-orbit heritage	600+ panels flown since 2008, 100% on-orbit success rate, LEO to GTO
Solar cell efficiency (historical)	~28% AM0 (early triple-junction cells)
Solar cell efficiency (current)	>32% AM0

$1 500

Pumpkin, Inc.

Lunar Rover Solar Panel

A custom PMDSAS solar array configured to the design constraints of a customer's lunar rover, with custom solar cell string configuration and ability to incorporate additional sens

Example configuration	72-cell, 6x10S1P + 1x12S1P solar panel
Example driven load	Pumpkin EPSM 1 with two 100Wh BM2 battery modules (not included)
Routing	Single-layer maze routing, no vias
Reliability features	Redundant current paths for every electrical node, strain-relieved interconnects, vacuum-b
Flight heritage	PMDSAS solar panel/solar array technology: 100% success rate in LEO and GTO orbits

price on request

Pumpkin, Inc.

Solar Panel Clips Set (Set of 8 clips)

A set of 8 low-mass clips for mounting up to six solar panels to the faces of a Pumpkin CubeSat Kit structure without shims.

Set size	8 clips
Thickness option 1	0.062"/1.6mm
Thickness option 2	0.031"/0.8mm
Compatibility	Pumpkin CubeSat Kit solid-wall or skeletonized structures (Base Plate Assembly / Cover Pla

$590datasheet

Pumpkin, Inc.

Solar Panel for AntS antenna

A flight-proven Pumpkin Modular Deployable Solar Array System (PMDSAS) fixed solar panel that replaces the default cover on the ISIS AntS antenna module, generating over 2W in AM0

SKU	710-00837
Price	$4,730.00
Classification	Flight Hardware | Flight Qualified | Space Proven
Panel thickness	0.024 in / 0.6 mm
Power output	over 2 W in AM0 conditions

$4 730

Redwire is an integrated aerospace and defense company that designs and manufactures advanced technologies for space and defense, including optical imaging, sun sensors, solar arrays, and spacecraft p

Redwire Corporation

Redwire HiPASS – High-Power Rigid Array Solution for SmallSats

SADA-compatible rigid solar array wing built for ESPA-class electric propulsion smallsat missions, using metallic tape-spring hinges.

Deployed wing dimensions	54 x 144 x 8 in (137 x 365 x 20 cm)
Stowed wing dimensions	30 x 54 x 7.5 in (76 x 137 x 19 cm)
Mass (1 kW point design)	17 kg
Electrical arrangement (1 kW point design)	19s20p per wing, Spectrolab XTE 76.88 cm^2 cells
Hinge type	Metallic tape-spring hinges

price on requestdatasheet

Redwire Corporation

Redwire Rigid Panel Solar Array Systems

Scalable rigid honeycomb-panel solar arrays from 50 W to over 15 kW per wing for LEO, MEO, GEO, and deep-space missions.

Power generation	50 W to >15 kW per wing
Specific mass	0.02-0.15 kg/W
Panel dimensions	~1 m x 1 m and larger, scaled to power
Construction	Composite facesheet, aluminum honeycomb, titanium inserts
Photovoltaic suppliers	Spectrolab, SolAero, Azur, Mpower

price on request

Redwire Corporation

Rigid Panel Solar Array

Heritage-proven deployable rigid panel solar arrays using high-efficiency triple-junction cells for LEO, MEO, and GEO spacecraft across commercial, civil, and defense programs.

Array Type	Rigid panel, deployable
Cell Technology	High-efficiency triple-junction
Orbit Applicability	LEO, MEO, GEO
Deployment	Spring-actuated hinged panel stack
Power Range	Scalable; mission-specific

price on request

Redwire Corporation

ROSA Roll-Out Solar Array

Redwire Corporation is a US space infrastructure and manufacturing company formed from the merger of multiple space companies including DSS (Deployable Space Systems, the inventor

price on request

Redwire is an integrated aerospace and defense company that designs and manufactures advanced technologies for space and defense applications, including space infrastructure, autonomous systems, and m

Roccor (Redwire)

ROSA — Roll-Out Solar Array

The Roll-Out Solar Array (ROSA) is Redwire’s flagship solar power product, a flexible, rollable photovoltaic array that deploys on-orbit via stored strain energy in its compo

ROSA Diamond	BOL power 3.3 kW; mass 36 kg; deployed length 8.6 m; stowed width 2.32 m
ROSA Opal	BOL power 5.3 kW; mass 42.7 kg; deployed length 12.6 m; stowed width 2.67 m
ROSA Sapphire	BOL power 12.9 kW; mass 160 kg; deployed length 21.2 m; stowed width 3.35 m
ROSA Tanzanite	BOL power 17.6 kW; mass 180 kg; deployed length 24.8 m; stowed width 4.15 m
ROSA SunStone	BOL power 28 kW; mass 331 kg; deployed length 19.4 m; stowed width 3.1 m

price on request

Rocket Lab designs and manufactures high-efficiency space solar power solutions, including solar cells and panels, for various spacecraft and missions, alongside providing launch services and other sa

SolAero Technologies (Rocket Lab)

Space Solar Solutions

Rocket Lab's Space Solar Solutions offer high-efficiency, radiation-hardened solar cells and customizable solar panel arrays to power spacecraft for various missions, from LEO to d

Solar Cell Efficiency	Up to 34%
Standard Cell Area	Up to 81.5 cm²
Flight-Proven Solar Cell Technologies	Triple-junction (ZTJ, ZTJ+ & ZTJ-Ω), Quad-junction (Z4J & Z4J+), Five-junction (IMM-β)
Solar Panel Options	Rigid and Flexible
Solar Panel Offerings	Rigid space photovoltaic solar panel assemblies (PVA), solar panel substrates, solar power

price on request

Colorado-based manufacturer of spacecraft solar arrays and modules at 10x lower cost than legacy systems, with flight heritage on SpaceX Transporter missions.

Source Energy

Large Deployable Solar Arrays

Source Energy’s Large Deployable Solar Arrays are designed for high-power rideshare spacecraft requiring multi-kilowatt power budgets. The architecture features aluminium or

Boom material	Aluminium or Carbon Fibre Pantograph
Deployment mechanism	Strain energy driven
Blanket fold	Z-folded photovoltaic blanket
Hold down	4 HDRMs and 8 kinematic mount interfaces
Structure	CFRP facesheet and aluminium honeycomb blanket box

price on request

Source Energy

Solar Modules

Source Energy’s Solar Modules are flight-proven space-qualified photovoltaic cells and subassemblies designed for extreme reliability in the space environment. With specific

Specific power	up to 303 W/kg
Electrical redundancy	Full
Micrometeorite tolerance	Yes
Shading tolerance	Localised shading tolerant
Materials	Space stable (UV, radiation, atomic oxygen hardened)

price on request

Slovak-Czech full-service nanosatellite mission provider offering CubeSat platforms (1U-16U), onboard subsystems, rideshare launch integration, and ground segment services.

Spacemanic s.r.o.

Ra

Ra is Spacemanic’s high-efficiency solar panel solution, engineered for nanosatellites and beyond, delivering reliable, mission-optimized energy for any platform size.

Flight heritage	Yes
ITAR free	Yes
Operating temperature	-40°C to +125°C
Efficiency	> 30%
Configurations	1U, 2U, 3U, 6U, 8U + customized design

price on requestdatasheet

Spacemanic s.r.o.

Ra Solar Panels

High-efficiency (>30%) custom solar panels for nanosatellites and small satellites, tailored to any CubeSat structure from 1U to 8U with premium solar cells.

Solar cell type	Premium triple-junction GaAs
Efficiency	> 30%
Panel sizes available	1U to 8U configurations
Operating temperature	–40 °C to +125 °C
Customization	Panel size, solar cell type, MPPT software — fully custom

$24 001 187 008

German space company designing, developing and producing solar arrays, laser-optical instruments and space electronics for satellite missions.

SpaceTech GmbH

SpaceTech Deployable Solar Arrays

One-stop deployable and body-mounted solar array solution with in-house panel manufacturing and multi-hinge deployment mechanisms.

Fill ratio	85%
Panel size range	< 0.5 m² (XS) to > 6 m² (XL) per panel
Deployment technology	Controlled, unsynchronized multi-hinge deployment using standardized C-spring hinges
Manufacturing	In-house panel manufacturing with automated photovoltaic cell laydown
Product scope	Body-mounted panels, single-hinge deployable arrays, multi-hinge deployable solar array wi

price on requestdatasheet

SpaceTech GmbH

SpaceTech SADA 44/22 (Solar Array Drive Assembly)

Integrated Solar Array Drive Assembly combining drive mechanism and drive electronics for LEO satellite constellations.

Driving method	Current controlled, micro stepping
Command interface	UART (57.6kBaud); RS-422 or RS-485 available
Supply voltage	22V … 36V
Standby current	<= 25 mA
Max load current	< 0.3 A

price on request

Manufacturer of high-efficiency multi-junction solar cells and solar arrays for spacecraft and remote sensing systems.

Spectrolab

Space Solar Arrays

Fully integrated and tested space solar arrays delivered to satellite primes for direct spacecraft integration, manufactured with Spectrolab's advanced multijunction cells and 70+

Integration	Fully integrated and tested — delivered assembly-ready
Cell Technology	XTE and XTJ family multijunction cells
Test Capability	LAPSS II large area pulsed solar simulator (up to 12 ft diameter panels)
Flight Heritage	500+ spacecraft including GEO, LEO, scientific, and defense missions
Heritage	70+ years of Spectrolab space solar array manufacturing

price on request

Spectrolab

XTE-HF Solar Cell

Spectrolab's XTE High Fluence 32% BOL triple-junction solar cell for MEO and very high radiation environments exceeding 1e15 fluence, achieving 23.6% efficiency at 1e16 fluence.

BOL Efficiency	32%
EOL Efficiency at 1e16 fluence	23.6%
Cell Technology	GaInP/GaAs/Ge lattice matched triple-junction (3J)
Qualification Standard	AIAA-S111-2014
Target Orbit	MEO (>1e15 fluence, Van Allen belt)

price on requestdatasheet

Spectrolab

XTE-LILT Solar Cell

Spectrolab's triple-junction solar cell optimized for Low Intensity Low Temperature conditions, achieving 37% efficiency at Jupiter for deep space missions to outer planets.

BOL Efficiency (1 AU)	32%
Efficiency at Jupiter LILT conditions	37%
Cell Technology	GaInP/GaAs/Ge lattice matched triple-junction (3J)
Qualification Standard	AIAA-S111-2014
Target Missions	Deep space (Jupiter and beyond, LILT conditions)

price on requestdatasheet

Spectrolab

XTE-SF Solar Cell

Spectrolab's XTE Standard Fluence 32% BOL triple-junction solar cell for GEO and LEO missions up to 1e15 fluence, qualified under AIAA-S111-2014.

BOL Efficiency	32%
EOL Efficiency at 1e15 fluence	27.9%
Cell Technology	GaInP/GaAs/Ge lattice matched triple-junction (3J)
Qualification Standard	AIAA-S111-2014
Target Orbit	GEO and LEO (≤1e15 fluence)

price on requestdatasheet

Spectrolab

XTE+ GEO Solar Cell

Spectrolab's latest 33% BOL efficiency triple-junction solar cell optimized for GEO and high-radiation missions (>1e14 fluence), fully qualified under AIAA-S111-2014.

BOL Efficiency	33%
EOL Efficiency at 1e15 fluence	28.5%
Cell Technology	GaInP/GaAs/Ge lattice matched triple-junction (3J)
Qualification Standard	AIAA-S111-2014
Target Orbit	GEO (>1e14 fluence)

price on requestdatasheet

Spectrolab

XTE+ LEO Solar Cell

Spectrolab's 33% BOL efficiency triple-junction solar cell optimized for LEO missions with lower radiation fluence (<1e14), achieving 30.6% efficiency at 1e14 fluence.

BOL Efficiency	33%
EOL Efficiency at 1e14 fluence	30.6%
Cell Technology	GaInP/GaAs/Ge lattice matched triple-junction (3J)
Qualification Standard	AIAA-S111-2014
Target Orbit	LEO (<1e14 fluence)

price on requestdatasheet

Spectrolab

XTJ Prime Solar Cell

Spectrolab's proven heritage triple-junction solar cell with 30.7% average BOL efficiency, dual-qualified under AIAA-S111 and AIAA-S112, available in sizes from 26 to 84 cm².

BOL Efficiency (average)	30.7%
EOL Efficiency at 1e15 fluence	26.7%
Cell Technology	Heritage upright lattice matched XTJ triple-junction
Qualification Standards	AIAA-S111 and AIAA-S112 (dual qualified)
Available Sizes	26–84 cm²

price on requestdatasheet

SPUTNIX is a Russian manufacturer of nanosatellite and microsatellite platforms, onboard subsystems and ground infrastructure, operating as a subsidiary brand of Sitronics Group.

SPUTNIX

CubeSat GaAs End/Edge Solar Panel SXC-SGE-03

GaAs solar panel with integrated electromagnetic coil for CubeSat top/bottom edges. 98×98 mm, 28% efficiency, 480–520 mA Isc, 37 g. Center aperture for sun sensors.

Dimensions	98 × 98 × 10 mm
Mass	37 g
Cell efficiency	28%
Open circuit voltage	5.0–5.5 V
Short circuit current	480–520 mA

price on request

SPUTNIX

CubeSat GaAs Side Solar Panel SXC-SGS-03

GaAs solar panel with built-in electromagnetic coil for CubeSat side surfaces. 98×82.6 mm, 28% efficiency, 480–520 mA Isc, 30 g. Scalable for 2U and 3U frames.

Dimensions	98 × 82.6 × 8.6 mm
Mass	30 g
Cell efficiency	28%
Open circuit voltage	5.0–5.5 V
Short circuit current	480–520 mA

price on request

SPUTNIX

GaAs end edge solar panel with coils

A GaAs solar panel with a built-in electromagnetic coil designed for CubeSat top/bottom edges, with a central aperture for sun sensors or small payloads (SXC-SGE-03).

Model	SPUTNIX SXC-SGE-03
Feature	Compatible with SPUTNIX SXC1 and SXC3 CubeSat frames
Feature	Diode protection circuit
Feature	Built-in planar coil
Feature	Scalable power and coils using several panels

price on request

SPUTNIX

GaAs side solar panel with coils

A GaAs solar panel with a built-in electromagnetic detumbling coil, sized for CubeSat side surfaces (SXC-SGS-03).

Model	SPUTNIX SXC-SGS-03
Feature	Compatible with SPUTNIX SXC1 and SXC3 CubeSat frames
Feature	Diode protection circuit
Feature	Built-in planar coil
Feature	Scalable power and coils using several panels

price on request