Power Systems

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

2NDSpace Srl

CORE Solar Panels

CORE is a series of body-mounted CubeSat solar panels from 2NDSpace, designed for reliable power generation with flight heritage.

Type	Body-mounted
Variants	CORE-01, 01Z, 02, 03, 06Z, 08, 12, 12Z, 16
Compatible Form Factors	1U to 16U

price on requestdatasheet

2NDSpace Srl

DROP Deployable Solar Panels

Deployable CubeSat solar panels from 1U to 16U with dual, triple or multi-wing configurations.

Form factor range	1U to 16U
Configuration	Dual, triple, or multi-wing
Solar cells	Single-sided or double-sided option
Design	Modular

price on request

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

2NDSpace Srl

DROP-08 8U/4U Deployable Solar panel

The DROP-08 is a deployable solar panel system designed for 8U/4U CubeSats, offering up to 30W of power with options for backstring and body-mounted configurations.

Deployable elements	1
Deployment Configuration	135°/90°
Front side power	10 W
Backstring option	+10W
Body mounted option	+10W

price on requestdatasheet

2NDSpace Srl

DROP-12 12U Deployable Solar panel

The DROP-12 is a 12U deployable solar panel system designed for CubeSats, offering up to 60W of peak power with options for backstring and body-mounted configurations.

Deployable elements	1
Deployment Configuration	135°/90°
Front side power	20 W
Backstring option	+20W
Body mounted option	+20W

price on requestdatasheet

2NDSpace Srl

SOLO Cubesat EPS

End-to-end power module for nanosatellites, combining power distribution, battery management and solar array conditioning.

Form factor range	1U to 27U
Functions	Power distribution, battery management, solar array conditioning
Architecture	Fault-tolerant, integrated PDCU
Battery packs	Modular, reconfigurable
Flight heritage	Yes

price on request

World-leading manufacturer of space electronic components using proprietary 3D interconnect technology for extreme miniaturization.

3D Plus (HEICO)

Latch-Up Current Limiter (LCL)

Radiation-hardened latch-up current limiter (3DPM0168) for space, monitoring 0.8–5.5V supply lines up to 2A with 10 μs switch-off on overcurrent or SEL event. SOP20 packaged with a

Part Number	3DPM0168
Voltage Range	0.8V to 5.5V
Maximum Current	2A
Switch-off Time	10 μs maximum
Temperature Range	-40°C to +115°C

price on request

3D Plus (HEICO)

Rad-Hard DDR Termination Regulator

Space-qualified radiation-hardened termination regulators for DDR2/3/4 memory buses (3DPM0237/0318/0385/0424), providing ±1A or ±2A with low noise and fast transient response. SOP2

3DPM0237 (DDR2) Input Voltage	1.6V to 2.8V
3DPM0237 Output Current	±1A
3DPM0237 Package	SOP24
3DPM0318 (DDR2) Input Voltage	1.6V to 2.8V
3DPM0318 Output Current	±1A

price on request

3D Plus (HEICO)

Space Point-of-Load (POL) DC/DC Converter

Space-qualified radiation-hardened point-of-load DC/DC converters in three variants (3DPM0211, 3DPM0289, 3DPM0602) covering 4.5–13.2V input and 0.8–5V adjustable output. 16-pin or

3DPM0211 Input Voltage	5V ±10%
3DPM0211 Output Voltage	1.225V to 3.8V (adjustable)
3DPM0211 Package	14-pin Gull Wing SMD
3DPM0289 Input Voltage	4.5V to 12V
3DPM0289 Output Voltage	1V to 5V (adjustable)

price on request

3D Plus (HEICO)

Space Radiation Hardened Protection Switch

Radiation-hardened protection switch (3DPM0356) for space power distribution, monitoring supply lines up to 7A at 3–12V and switching off in 20 μs on overcurrent detection. BGA48 p

Part Number	3DPM0356-1
Input Voltage Range	3V to 12V
Maximum Line Current	7A
Voltage Drop	90 mV at 7A
Switch-OFF Time	20 μs maximum

price on request

AAC Clyde Space provides small satellite technologies and space-based data services, offering end-to-end solutions from satellite components to data analytics for various applications.

AAC Clyde Space

CubeSat EPS – STARBUCK-Nano

Flight-proven electrical power system for 3U-16U CubeSats featuring Maximum Power Point Tracking and robust reliability with TRL 9 maturity.

Design Life	5 years in LEO
Regulated Power Buses	3.3V; 5V; and 12V
Latching Current Limit (LCL)	10 Configurable
Interfaces	I2C
Max. Battery Voltage	8.2V

price on requestdatasheet

AAC Clyde Space

OPTIMUS Battery

The OPTIMUS Battery is a highly reliable and scalable CubeSat battery range with extensive flight heritage, featuring integrated thermostatically controlled heaters and multiple pr

TRL	9
Flown Since	2014
Available Capacities	30, 40 & 80 Whr
Battery Type	High quality lithium-ion battery
Qualification	Qualified to NASA standards EP-Wi-032

price on requestdatasheet

AAC Clyde Space

PHOTON CubeSat Solar Arrays

The PHOTON CubeSat Solar Arrays are a range of highly reliable, low-mass solar panels designed for maximum power generation and ease of integration into CubeSat platforms, compatib

Telemetry available	Temperature Sensors & Coarse Sun Sensors
Cell Type	XTJ Prime (others available on request)
Power Generation	Up to 9W per 3U populated face
Operating Temperature Range	-40°C to +80°C
PHOTON-DD - 3U Size Only Stowed height	9.55mm

price on requestdatasheet

AAC Clyde Space

SmallSat PCDU – STARBUCK-MINI

The STARBUCK-MINI is a SmallSat Power Conditioning and Distribution Unit (PCDU) designed for high-performance power control across various missions. Upgraded to deliver 2.5 kW of s

Design Life	5-7 years in LEO
System Power	2.5 kW
Primary Bus Voltage	22-34 V
Solar Power Regulation	MPPT or S3R
Battery Charge Regulation	CC-CV

price on request

AAC Clyde Space

SmallSat PCDU – STARBUCK-Mini MCC

An advanced SmallSat PCDU with an integrated Mission Control Computer, combining power management and satellite OBC functions into a single unit for streamlined satellite architect

Design Life	5-7 years in LEO
System Power	2.5 kW
Primary Bus Voltage	22-34 V
Solar Power Regulation	MPPT or S3R
Battery Charge Regulation	CC-CV

price on request

AAC Clyde Space

STARBUCK-NANO CubeSat EPS

The STARBUCK-NANO is a flight-proven Electrical Power System (EPS) for CubeSats, supporting 2U to 16U missions with features like Maximum Power Point Tracking and multiple protecti

Max power voltage	8.2V
Regulated power buses	3.3V, 5V, 12V
Power Distribution Modules	10 Latching Current Limiters
Supported CubeSat sizes	2U to 16U (STARBUCK-NANO for 2U/3U body-mounted, STARBUCK-NANO PLUS for 3U deployable up t
Optimization	Low Earth Orbit (LEO)

price on requestdatasheet

Airbus Defence and Space designs and manufactures satellites, spacecraft equipment, and provides related services for telecommunications, navigation, Earth observation, and space exploration.

Airbus Defence and Space

Airbus Space Battery Products

Airbus offers four product lines of space-qualified Lithium-Ion batteries (ASTRO-BATT, COSMO-BATT, STELLAR-BATT, LAUNCHER-BATT) designed for diverse space missions, from LEO conste

ASTRO-BATT Voltage Configurations	30, 50 and 100V
ASTRO-BATT Qualification	Successfully qualified mid-2024
COSMO-BATT Single Module Energy Range	500 to 3000 Wh
COSMO-BATT-S Energy	From 500 to 1000 Wh
COSMO-BATT-S Flight Heritage	On board on Galileo satellites

price on requestdatasheet

Airbus Defence and Space

Power Conditioning and Distribution Units (PCDU)

Airbus offers advanced power conditioning and distribution units (PCDUs) optimized for space applications, ensuring reliable power conversion, regulation, and distribution for spac

Product	PSR 100V MKII
Qualification	Fully qualified
Fault Tolerance	Fault tolerant
Availability	Off the shelf unit
Development Origin	AIRBUS Defence and Space for telecom satellites under ESA initiative

price on requestdatasheet

Airbus Defence and Space

PSR 100V MKII

A fully qualified, fault-tolerant power supply regulator developed by Airbus Defence and Space for telecom satellites under an ESA initiative, handling up to 23kW at 100V.

Power handling capacity	up to 23kW at 100V
Flight heritage	Alphabus, E3000, E3000-NEO, Galileo; legacy from PSR 50V with more than 80 units in flight

price on requestdatasheet

Airbus Defence and Space

PureLine Topaz/THORs

A compact, end-to-end power processing unit subsystem for satellite electric propulsion, developed for New Space and constellation applications with a 10-year LEO lifetime.

Lifetime	10 years in LEO
Electronic parts	Latch-up-free with error protection
Applications	Orbit raising, station-keeping, deorbiting
Product line	PureLine (New Space catalogue avionics)

price on requestdatasheet

Alba Orbital manufactures PocketQube satellites, provides launch and ground station services, and operates a fleet of nighttime imaging satellites for government and commercial clients.

Alba Orbital

Solar Panels 1p Set (QTY 5)

A set of five solar panels designed for PocketQubes, featuring high-efficiency Spectrolab TASC cells and custom mounting holes.

Set of	5
Available for	1p/2p/3p PocketQubes
Cells	Spectrolab high efficiency TASC
PCB	Low thickness polyimide substrate
Solar module fabricated under	ECSS-Q-ST-70-08 and ECSS-E-ST-20-08 requirements

price on requestdatasheet

Ananth Technologies is a Hyderabad-based aerospace and defence company that partners with ISRO and DRDO on satellite assembly, integration and testing, launch vehicle electronics, and RF/microwave systems.

Ananth Technologies

Solar Panels

Ananth Technologies designs and manufactures high-performance solar panels for satellites ranging from CubeSats to advanced microsatellites, combining flight-proven materials, prec

Cell Type	Triple-junction GaAs
Efficiency	Up to 31%
Operating Temp	-60°C to +110°C
Radiation Tolerance	1E15 e/cm²
Mission Life	15+ years

price on request

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

Italian picosatellite manufacturer and IoT connectivity provider building 0.3U–6U CubeSat platforms and antennas for agricultural, industrial, maritime, and environmental monitoring applications.

Apogeo Space

Solar Panels for Picosatellites

High-efficiency solar panels optimized for picosatellite platforms to maximize energy output and ensure reliable power generation throughout the mission.

Compatible Platforms	0.3U, 1U, 3U, 6U CubeSat
Configuration	Body-mounted or deployable
Standard	CubeSat Specification

price on request

Argotec is an Italian spacecraft manufacturer that designed and operates the ArgoMoon CubeSat and develops satellite platforms and subsystems for ESA and commercial missions.

Argotec Srl

EBC Rad-Hard External Battery Charger

Radiation-hardened external battery charger that automates microsatellite battery management during long cruise phases to the Moon, Mars or asteroids.

Type	External Battery Charger (EBC), rad-hard
Function	Automated battery management during long cruise phases
Target destinations	Remote locations such as the Moon, Mars and asteroids
Integration	Safe integration with a mothercraft, with fault isolation
Embedded functions	Battery charge regulation; thermal control off-loading in survival and operative (charging

price on request

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

Berlin Space Technologies (BST) designs and mass manufactures small satellite systems and technologies, providing end-to-end solutions for space missions.

Berlin Space Technologies

BAT-110

The BST BAT-110 is a modular Li-Fe battery system for small satellites, offering high cycle life, safety features, and customizable voltage and capacity.

Voltage	23.1V (customizable)
Capacity	7.5Ah (customizable)
Operating Temperature	-20°C to 40°C
Storage Temperature	-30°C to 50°C
Protection	Overvoltage, Undervoltage

price on requestdatasheet

Berlin Space Technologies

PCU-110

The PCU-110 by Berlin Space Technologies is a power control unit for small satellites, providing power regulation, switching, DC/DC conversion, and safety features.

Data Interfaces	RS422, I²C
Solar Panel Interface	12x 23.1V (customizable)
Battery Interface	6x 23.1V (customizable)
Bus Voltage	23.1V (customizable)
Regulated Voltages	12V, 5V, 3.3V (customizable)

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

High Capacity Batteries

Blue Canyon Technologies offers high-capacity batteries with integrated heaters to optimize operation at low temperatures, available in two configurations: IP8S and 2P8S.

IP8S Nameplate Capacity	3.4 Ah
IP8S Energy	99 Wh
IP8S Mass	<650 g
2P8S Nameplate Capacity	6.8 Ah
2P8S Energy	198 Wh

price on requestdatasheet

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

Swedish green propulsion pioneer; HPGP / LMP-103S thrusters using ADN propellant with 12% higher Isp than hydrazine; Bradford ENOVIA group.

Bradford Space

Supernova High Power PCDU

High-power power conditioning and distribution unit for deep-space avionics and demanding satellite bus power architectures.

Product Category

Deep Space Avionics

price on request

Hungarian manufacturer of small satellite platforms, subsystems, and mission services with a 100% mission success rate, serving NewSpace and traditional satellite markets.

C3S LLC

Electrical Power System (EPS) 2000

The EPS 2000 is a complete power supply solution for CubeSats and Small Satellites, featuring single point failure tolerance, redundant CAN bus communication, and high efficiency G

Current Development Stage	TRL4, aiming for TRL7 by Q2 2026.
Input voltage range	6 to 70 V
Output voltage	5V, 12V, Unregulated 28V
Peak output power	2 kW
Battery capacity	Up to 2 kWh

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

Scottish CubeSat and small satellite manufacturer in Glasgow, founded 2005; 100+ satellites launched; EPS, OBC, ADCS, structural, and propulsion subsystems for nanosats and microsats; acquired by AAC Microtec (now AAC Clyde Space).

Clyde Space

CubeSat Electrical Power Systems and Smallsat Platforms

Clyde Space (now AAC Clyde Space, following acquisition by Swedish company AAC Microtec in 2019) is a Scottish CubeSat and smallsat manufacturer based in Glasgow. The company is on

price on request

Clyde Space

CubeSat Power Systems (EPS and Batteries)

Clyde Space's flight-proven CubeSat electrical power systems (EPS), lithium polymer batteries, and power conditioning units for 1U–12U satellite platforms.

Products	EPS (1U–12U), LiPo batteries, solar panel MPPT, power distribution
Power Buses	+3.3V, +5V, +12V regulated rails
Battery Temp Range	-20°C to +60°C (space-qualified)
Lifetime	3–5 year design lifetime
Heritage	Hundreds of CubeSat missions (NASA, ESA, Planet, Spire, JAXA, others)

price on request

Chinese state-owned nuclear enterprise founded 1955 in Beijing overseeing civilian nuclear power, fuel production, and uranium mining; uses satellite remote sensing for exploration and researches nuclear space propulsion.

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

Crystal Space designs and manufactures cameras and smart cameras for satellites, rovers, landers, and UxS, with over 200 cameras delivered and 12,500+ collective days in space.

Crystal Space

Crystalspace P1U “Vasik”

The Crystalspace P1U EPS is an advanced power supply designed for 1U and 2U CubeSats, featuring fast MPPT boost converters and a duplicated battery pack.

Manufacturer	CrystalSpace
Lead time	6 – 8 weeks

price on request

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 Battery Board

The 1U Battery Board by CubeSat Aerospace is a compact, high-efficiency energy storage module designed for small satellite missions, supporting regulated power delivery and offerin

Battery Type	Li-ion (18650 cells or flat-pack pouch, configurable)
Nominal Voltage	3.7 V – 7.4 V (single or dual cell configuration)
Capacity Range	2600 mAh – 5200 mAh (standard configurations)
Charging Method	MPPT solar input or USB-C interface via avionics board
Protection Features	Overcharge, over-discharge protection; Short circuit and overcurrent protection; Thermal c

price on request

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

Vertically integrated Indian defence and aerospace electronics company designing and manufacturing avionics, microelectronics, RF/microwave, radar, test equipment and space systems.

Data Patterns (India) Ltd.

Power Supply (Various Models)

Data Patterns India develops a range of power supplies for air, naval, ground-based, and space applications, available in VPX, VME, cPCI, and custom form factors.

Product Name	DP-ATE-8033
Description	Shaker Table Power Supply
Product Name	DP-ATE-8219
Description	ATS Power Module
Product Name	DP-FCS-8110

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

Dcubed

Rigid-Deployable Solar Array

Dcubed's rigid-deployable solar array offers a modular, compact, and lightweight solution for maximizing power generation in space applications.

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

Electrical Power Systems (EPS)

DHV Technology offers a range of Electrical Power Systems (EPS) including PCDU for SmallSats, NanoEPS for 3U to 6U CubeSats, PicoEPS for 1U to 2U CubeSats, and MicroEPS for 6U to 1

PCDU Power Module Scalability	starting at 900W
PCDU Battery Module Capacity	415Wh ~ 1660Wh
NanoEPS CubeSat Compatibility	non-deployable 3U to triple deployable 2U, 3U or 6U
NanoEPS Power Bus Generation	3.3V, 5V, 12V and VBAT
NanoEPS Form Factor	PC104

price on request

DHV Technology

Solar Array Drive Assembly (SADA)

The Solar Array Drive Assembly (SADA) is a mechanism for rotating solar arrays on CubeSats and SmallSats to maintain optimal sun orientation and transfer power to the satellite bus

price on request

DHV Technology

Solar Panels for CubeSats

Body-mounted solar panels for 1U, 2U, 3U, 6U, 12U, and 16U CubeSats with high-efficiency triple-junction solar cells and qualified for LEO missions.

price on request

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

Emxys is a Spanish space electronics company specialising in advanced onboard computers, power systems, optical transceivers, and complete nanosatellite platforms for data-intensive space missions.

Emxys

ODALISS PDCU

The ODALISS PDCU is a highly efficient Power Distribution and Control Unit designed for space avionics, featuring redundant Solar Array Regulators with MPPT and comprehensive batte

Battery Pack Configuration	Dual 2s1p Li-Ion battery
Nominal voltage per battery	+7.4V
Fully charged voltage per battery	+8.2V
Fully charged current per battery	1A
Maximum discharge current per battery	8A

price on requestdatasheet

Emxys

ODALISS Solar Panels

The ODALISS Solar Panels are highly efficient 3U/6U CubeSat compatible solar panels equipped with the latest triple junction technology and integrated temperature and sun sensors.

Cell efficiency	higher than 29%
Sensors	Integrated active linear temperature transducer.
Sensors	High sensitivity Silicon photodiode included.
Connectors	Three 4-pin solar array power output for flexible panels interconnection.
Connectors	One 4-pin for temperature sensor.

price on requestdatasheet

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

EnduroSat

CubeSat EPS

EnduroSat's Electrical Power System (EPS) for CubeSats, supporting a battery pack module with 1100 Wh capacity per package.

Battery Pack Capacity

1100 Wh per package

price on request

EnduroSat

SmallSat EPS

High-efficiency, modular Electrical Power System for advanced small satellite missions. Combines large battery packs with multi-bus power distribution to deliver hundreds of amps o

Battery Pack Capacity	1100
System Bus (vBatt)	30-50
Regulated Power Buses	12, 28
Max Continuous Current (28V)	125
Input Voltage	up to 70

price on request

Global leader in stored energy solutions — ABSL Space Products division delivers lithium-ion battery systems for spacecraft, used on Rosetta, Cassini, and numerous ESA missions.

EnerSys / ABSL Space Products

ABSL CM1040 36s4p Li-ion Space Battery (126 V, 8 Ah)

Fully qualified 1066 Wh Li-ion space battery in 36s4p topology, used on launch vehicles including for Thrust Vector Control, 8.4 kg.

Cell	ABSL P20
Topology	36s4p
Voltage range	151.2 - 108.0 V
Nameplate capacity	8 Ah
Energy	1066 Wh

price on requestdatasheet

EnerSys / ABSL Space Products

ABSL CM1040 8s18p Li-ion Space Battery (28 V, 36 Ah)

1066 Wh Li-ion space battery in 8s18p topology on a 28 V bus, 36 Ah nameplate capacity, 8.8 kg.

Cell	ABSL P20
Topology	8s18p
Voltage range	33.6 - 24.0 V
Nameplate capacity	36 Ah
Energy	1066 Wh

price on requestdatasheet

EnerSys / ABSL Space Products

ABSL CM170 4s6p Li-ion Space Battery (14 V, 12 Ah)

Compact 178 Wh Li-ion space battery in 4s6p topology for a 14 V bus, 1.6 kg, suited to SmallSat missions.

Cell	ABSL P20
Topology	4s6p
Voltage range	16.8 - 12.0 V
Nameplate capacity	12 Ah
Energy	178 Wh

price on requestdatasheet

EnerSys / ABSL Space Products

ABSL CM230 8s4p Li-ion Space Battery (28 V, 8 Ah)

236.8 Wh Li-ion space battery in 8s4p topology for a 28 V bus, 2.05 kg.

Cell	ABSL P20
Topology	8s4p
Voltage range	33.6 - 24.0 V
Nameplate capacity	8 Ah
Energy	236.8 Wh

price on requestdatasheet

EnerSys / ABSL Space Products

ABSL CM2300 16s20p Li-ion Space Battery (56 V, 40 Ah)

2300 Wh Li-ion space battery in 16s20p topology for a 56 V bus, 40 Ah nameplate capacity, 19.6 kg.

Cell	ABSL P20
Topology	16s20p
Voltage range	67.2 - 48.0 V
Nameplate capacity	40 Ah
Energy	2300 Wh

price on requestdatasheet

EnerSys / ABSL Space Products

ABSL CM2300 8s40p Li-ion Space Battery (28 V, 80 Ah)

2300 Wh Li-ion space battery in 8s40p topology for a 28 V bus, 80 Ah nameplate capacity, 20 kg.

Cell	ABSL P20
Topology	8s40p
Voltage range	33.6 - 24.0 V
Nameplate capacity	80 Ah
Energy	2300 Wh

price on requestdatasheet

EnerSys / ABSL Space Products

ABSL CM520 8s9p Li-ion Space Battery (28 V, 18 Ah)

532.8 Wh Li-ion space battery in 8s9p topology for a 28 V bus, 4.3 kg.

Cell	ABSL P20
Topology	8s9p
Voltage range	33.6 - 24.0 V
Nameplate capacity	18 Ah
Energy	532.8 Wh

price on requestdatasheet

US manufacturer of non-explosive actuators (TiNi FrangiBolt, pin pullers, ejectors) and energetic hold-down and release systems.

Ensign-Bickford Aerospace & Defense (EBAD)

NEA® 8020 Series Battery Cell Bypass Switch

An electrically initiated, one-shot switch designed to bypass and isolate failed battery cells, featuring Make-Before-Break functionality and available in non-autonomous and autono

Continuous Current Ratings	100 A
Switch Resistance	<200 μΩ @ 100 A
Fuse Wire Resistance	0.5 to 1.6 Ω @ 25°C
Minimum Actuation Current	1.2 A
Nominal Actuation Current	4 Amps for 25 ms

price on request

Ensign-Bickford Aerospace & Defense (EBAD)

NEA® 8030 Series Battery Cell Bypass Switch

An electrically initiated, one-shot switch designed to bypass and isolate failed battery cells, featuring Make-Before-Break functionality and available in non-autonomous and autono

Continuous Current Ratings	250 A
Switch Resistance	<200 μΩ @ 250 A
Fuse Wire Resistance	0.5 to 1.6 Ω @ 25°C
Minimum Actuation Current	1.2 A
Nominal Actuation Current	4 Amps for 25 ms

price on request

Ensign-Bickford Aerospace & Defense (EBAD)

NEA® 8040 Series Battery Cell Bypass Switch

An electrically initiated, one-shot switch designed to bypass and isolate failed battery cells in battery assemblies, offering Make-Before-Break functionality.

Continuous Current Ratings	400 A
Switch Resistance	<150 μΩ @ 400 A
Fuse Wire Resistance	0.95 to 1.6 Ω @ 25°C
Minimum Actuation Current	1.2 A
Nominal Actuation Current	4 Amps for 25 ms

price on request

EREMS is a French SME founded in 1979, specializing in the design and realization of electronic equipment and software for high technology fields including Space.

EREMS

PCDU NANO Power Conditioning and Distribution Unit

Modular power system for nanosatellites (6U-27U) compliant with the CubeSat standard — SAM3X microcontroller, configurable MPPT/DET/distribution modules.

Microcontroller	SAM3X (Microchip)
CubeSat form-factor range	6U-27U
MPPT module	Up to 4x 12W solar sections per module, digital MPPT per channel
DET module	Up to 5x 20W solar sections per module (Direct Energy Transfer)
Distribution module	Up to 10W @5V and 6W @3.3V per module; up to 14x LCL-protected power lines

price on request

French SATCOM equipment distributor and integrator; ground station hardware across L to Q band; founded 2003 in Les Ulis.

EUROSATCOM

Space-Grade DC-DC Converters

Radiation-hardened DC-DC power converters and point-of-load regulators for spacecraft buses and cubesats — 2.5W to 500W, 12V-120V input options.

Maximum power output range	2.5W to 500W
Input voltage options	12 VDC (Cubesats), 28 VDC, 50 VDC, 70 VDC, 100 VDC, 120 VDC (Space Station)

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 BA0x High Energy Density Battery Array

As thin as 7 millimetres thick, the EXA BA0x High Energy Density Battery Array is a family of power store/delivery devices designed to provide the highest energy capacity and…

Manufacturer	EXA
Lead time	4 – 6 weeks

price on request

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

EXA (Ecuadorian Space Agency)

EXA TITAN-1 350Whr High Energy Density Battery Matrix

The EXA TITAN-1 350Whr High Energy Density Battery Matrix is a 1U-sized power bank module built from 7 battery arrays designed to provide the highest energy capacity and…

Manufacturer	EXA
Lead time	6 to 8 weeks

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

Flywheel Aerospace designs and manufactures modular robotics platforms and educational kits, serving universities, research labs, and startups in India with solutions for robotics, AI, and space techn

Flywheel Aerospace

Flywheel Energy Storage for Satellites

Flywheel Aerospace's kinetic energy storage systems — high-cycle-life flywheels for satellite power smoothing, peak power delivery, and combined energy/attitude control (momentum w

Technology	Carbon fiber composite flywheel, magnetic bearings, vacuum operation
Speeds	10,000–100,000 RPM
Dual Function	Energy storage + attitude control (IPACS concept)
Advantage	Unlimited charge-discharge cycles vs. battery degradation
Target Orbit	LEO (15 eclipses/day → battery killer, flywheel ideal)

price on request

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

Glavkosmos

ARC Regulation and Control Equipment for Manned and Cargo Spacecraft

The ARC Regulation and Control Equipment is a monoblock system designed for regulating and monitoring the power supply system of manned spacecraft, capable of operating in vacuum.

Purpose	Designed for manned spacecraft.
Year of release	2012
Guaranteed service life	5 years
Estimated production / delivery time	18 months
Flight qualification of the product	No

price on request

Glavkosmos

DC/DC Converter

Radiation-resistant secondary DC/DC converter on switched capacitors, similar to TPS605000/LM2771/LTC3250.

Input voltage	2.8–5.5 V
Output voltage	1.2–3.3 V
Output current	<300 mA
Efficiency	60–75%
Year of release	2014

price on request

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

High Voltage Power Supply System kit KPVS

The High Voltage Power Supply System kit KPVS is a modular power solution designed for large spacecraft and orbital station modules, capable of providing up to 60 kW of power.

Year of release	2014
Guaranteed service life	17 years
Estimated production / delivery time	18 months
Flight qualification of the product	No
Possibility to adapt the product to customer requirements	Yes

price on request

Glavkosmos

High-capacity Rechargeable Battery for Power Supply of Spacecraft and Ground Infrastructure

This is a high-capacity rechargeable battery designed for power supply applications in both spacecraft and ground infrastructure, offering a guaranteed service life of 5 years.

Year of release	2008
Guaranteed service life	5 years
Estimated production / delivery time	4 months
Possibility to adapt the product to customer requirements	No
Capacity	90 Ah

price on request

Glavkosmos

Nanosatellite Battery Array

The Nanosatellite Battery Array is a power storage solution for nanosatellites, featuring overcurrent, overcharge, and overdischarge protection.

Purpose	Battery array board designed to store power on nanosatellite.
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

Nanosatellite Electrical Power System

The Nanosatellite Electrical Power System is a board designed to provide power to nanosatellite systems and collect power from solar cells, featuring multiple constant and switchab

Year of release	2016
Guaranteed service life	1 year
Estimated production / delivery time	6 months
Flight qualification of the product	No
Possibility to adapt the product to customer requirements	Yes

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

Optical Glass

Optical Glass is a cerium-doped glass plate designed to protect solar cells from the harsh environment of outer space.

Dimensions L x W x H, mm

80,5 kh 40,5 kh 0,27 / 0,12 / 0,06 / 0,17

price on request

Glavkosmos

Power Supply System [with battery unit]

A power supply system designed for satellite subsystems, featuring three independent charger units with MPPT, multiple output channels, and support for various solar panel types.

Purpose	Designed for power supply of satellite subsystems.
Year of release	2018
Guaranteed service life	1 years
Estimated production / delivery time	2 months
Flight qualification of the product	Yes

price on request

Glavkosmos

Rechargeable Battery for Power Supply of Ground Infrastructure

A sealed rechargeable battery providing power for ground-based space infrastructure, offering 70 Ah capacity at 28.8 V nominal voltage with a 15-year guaranteed service life.

Year of release	2007
Guaranteed service life (years)	15
Estimated production / delivery time (months)	4
Possibility to adapt the product to customer requirements	No
Capacity, Ah	70

price on request

Glavkosmos

Rechargeable Battery for Power Supply of Spacecraft

This is a rechargeable battery designed for power supply of spacecraft, featuring a capacity of 90 Ah and a nominal voltage of 28.8 V.

Purpose	Power supply of spacecraft.
Year of release	1975
Guaranteed service life	2 years
Estimated production / delivery time	4 months
Possibility to adapt the product to customer requirements	No

price on request

Glavkosmos

Rechargeable Battery for Power Supply of Spacecraft and Ground Infrastructure

This is a rechargeable battery designed for power supply in both spacecraft and ground infrastructure, offering a capacity of 20 Ah and a nominal voltage of 23.8 V.

Year of release	2003
Guaranteed service life (years)	5
Estimated production / delivery time (months)	4
Possibility to adapt the product to customer requirements	No
Capacity, Ah	20

price on request

Glavkosmos

Regulation and Monitoring Equipment of Electric Power Supply System EPS) ARK-MKA

The ARK-MKA is a monoblock equipment designed for the regulation and monitoring of a spacecraft's electric power supply system, suitable for high-orbit missions.

Year of release	2015
Guaranteed service life	9 years
Estimated production/delivery time	18 months
Flight qualification of the product	No
Possibility to adapt the product to customer requirements	Yes

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

Glavkosmos

Solar Cell Battery

A solar cell battery designed for CubeSat spacecraft, serving as a primary component of the power supply system and part of a measurement and motion control complex satellite syste

Purpose	Generation of electricity for power supply system of CubeSat type spacecraft.
Year of release	2015
Estimated production / delivery time (months)	2
Flight qualification of the product	Yes
Possibility to adapt the product to customer requirements	Yes

price on request

Glavkosmos

Solar Element GaInP2 / GaAs / Ge

This is a triple-junction solar cell (GaInP2 / GaAs / Ge) designed for spacecraft solar power systems, converting solar energy into electrical power.

Purpose	Utilization in battery design of solar power supply systems of spacecraft to convert solar
Year of release	2007
Estimated production / delivery time	1 months
Flight qualification of the product	Yes
Possibility to adapt the product to customer requirements	Yes

price on request

Glavkosmos

Unified DC-DC Conversion Module

A compact DC-DC power conversion module that converts an unstable primary supply into a set of stabilized output voltages, forming part of a unified set of modules for critical pow

Purpose	Power Electronics, Energy
Year of release	2012
Guaranteed service life (years)	3
Estimated production / delivery time (months)	8
Flight qualification of the product	No

price on request

Glavkosmos

Unified Power Management and Control Module

A compact 32-bit RISC-based module for monitoring and controlling power sources in guaranteed/critical power systems, detecting fault conditions and reporting status via CAN and TT

Purpose	Power Electronics, Energy
Year of release	2012
Guaranteed service life (years)	3
Estimated production / delivery time (months)	8
Flight qualification of the product	No

price on request

Glavkosmos

Voltage Converter PN120/28

The Voltage Converter PN120/28 is a current and voltage regulator designed for spacecraft onboard equipment, converting 110-180 V DC to 28.5 V DC.

Purpose	Designed for manned and cargo spacecraft, satellites.
Year of release	2000
Guaranteed service life (years)	15
Estimated production / delivery time (months)	12
Flight qualification of the product	Yes

price on request

Glavkosmos

Voltage Converter PN28/120

The Voltage Converter PN28/120 is a flight-qualified power converter designed for spacecraft, converting 28.5 V DC to 120 V DC with 2 kW power output.

Purpose	Designed for manned and cargo spacecraft, satellites.
Year of release	2000
Guaranteed service life (years)	15
Estimated production / delivery time (months)	12
Flight qualification of the product	Yes

price on request

Glavkosmos

Voltage Converter Single-phase, Upgraded POS-80-RNM

The POS-80-RNM is an upgraded single-phase voltage converter designed for manned and cargo spacecraft, providing stable, high-precision AC power for onboard equipment.

Purpose	Designed for manned and cargo spacecraft.
Year of release	2013
Guaranteed service life	10 years
Estimated production / delivery time	6 months
Flight qualification of the product	No

price on request

GomSpace is a Danish CubeSat manufacturer producing satellite platforms, subsystems, and end-to-end mission solutions. Products include the NanoCom radio modules, NanoPower EPS, and complete 1U–12U satellite platforms. GomSpace has one of t

GomSpace

NanoPower P31u EPS

The NanoPower P31u is an Electrical Power System (EPS) module developed by GomSpace for 1U–3U CubeSats. It integrates solar panel inputs, battery management, power distribution, an

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

Turkish space and aerospace technology company; satellite engineering services, space system components, and technical expertise for Turkey's growing commercial space sector.

Gumush

NART-EPS Electric Power Subsystem (EPS)

NART-EPS is an Electric Power Subsystem (EPS) for satellites, utilizing supercapacitors for superior life cycle, depth of discharge, efficiency, and reliability.

Form Factor	PC-104 Bus Standard
Inhibit Switches	3x, for safe flight
PDM Switches	10x, for power distribution
MPPT	Maximum Power Point Tracking
Max Input Voltage	20 V (all BCR)

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

Howe Industries is a Scottsdale, Arizona propulsion startup developing advanced space technologies including ThermaSat water-propellant electrothermal CubeSat thrusters, nuclear pulsed plasma rockets, and orbital robotics, backed by NASA NI

Howe Industries

SPEAR Probe

Compact deep-space nuclear power and propulsion probe delivering 3 kW electric at 20% conversion efficiency over a 14-year mission, targeting CubeSat deployment to Europa and other

Electric power output	3 kW
Thermal power output	15 kW
Conversion efficiency	20%
Wet mass	1,540 kg
Payload capacity	70 kg

price on request

Ibeos designs and manufactures satellite electronics, including processors, single board computers, and electric power subsystems, for LEO, GEO, and beyond missions.

ibeos

B14-M45/M90 14V Modular SmallSat Battery

Radiation-tolerant 14V modular Li-ion SmallSat battery: 45 Whr single module (B14-M45) or 90 Whr dual module (B14-M90), 6.5A peak discharge, 30 kRad TID, TRL 9.

Configuration	B14-M45: 45 Whr (single); B14-M90: 90 Whr (dual module)
Nominal Voltage	13.2–16.8 V
Max Discharge Rate	6.5 A
Recommended Charge Rate	1.6 A
Heater Power	8 W @ 16V

price on request

ibeos

B28-135 28V SmallSat Battery

Radiation-tolerant 28V 135 Whr Li-ion SmallSat battery, 10A sustained discharge, 30 kRad TID, aluminum+PEEK chassis, 21-pin Micro-D connector, compatible with Ibeos E28-200 EPS.

Capacity	135 Whr
Voltage	22–33.6 V
Sustained Discharge Rate	10 A
Recommended Charge Rate	2.5 A
Heater Power	20 W @ 28V

price on request

ibeos

B28-M275/550/825/1100 28V Modular Battery Series

Scalable 28V modular Li-ion battery series in 275, 550, 825, and 1100 Whr configurations, 20–80A peak discharge, 30 kRad TID, aluminum+PEEK chassis, TRL 9.

Configurations	B28-M275 (275 Whr), B28-M550 (550 Whr), B28-M825 (825 Whr), B28-M1100 (1100 Whr)
Operating Voltage	24–33.6 V
Max Discharge Rate	20A (275 Whr) to 80A (1100 Whr)
Recommended Charge Rate	5A (275 Whr) to 20A (1100 Whr)
Mass Range	2.1–7.8 kg

price on request

ibeos

B50-412/825/1237 50V Modular Battery Series

Scalable 50V modular Li-ion battery series in 412, 825, and 1237 Whr configurations, 20–60A peak discharge, 30 kRad TID, aluminum+PEEK chassis, successor to B50-1000.

Configurations	B50-412 (412 Whr), B50-825 (825 Whr), B50-1237 (1237 Whr)
Operating Voltage	36–50.4 V
Max Discharge Rate	20A (412 Whr) to 60A (1237 Whr)
Recommended Charge Rate	5A (412 Whr) to 15A (1237 Whr)
Mass Range	3.0–8.8 kg

price on request

ibeos

E14-150 14V SmallSat Electric Power System

150W radiation-tolerant 14V SmallSat EPS with peak-power tracking, 96% solar array efficiency, 3.3V/5V/12V regulated buses, 10x switched outputs, I2C/SPI telemetry, 30 kRad TID, TR

Max Solar Array Input	>150W (18–42V input)
S/A Conversion Efficiency	96%
3.3V Output	3A (92% efficiency)
5V Output	6A (93% efficiency)
12V Output	4A (95% efficiency)

price on request

ibeos

E28-200 28V SmallSat Electric Power System

250W radiation-tolerant 28V SmallSat EPS with peak-power tracking, 96% solar array efficiency, 3.3V/5V/12V/28V buses, 10x switched outputs, RS-422/485/I2C/SPI, 30 kRad TID, TRL 9.

Max Solar Array Input	>250W (14–34V input)
S/A Conversion Efficiency	96%
3.3V Output	3A (92% efficiency)
5V Output	6A (93% efficiency)
12V Output	4A (95% efficiency)

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

ISISPACE provides launch services, manufactures CubeSat deployers and other launch equipment, and acts as a satellite systems integrator for small satellites.

Innovative Space Logistics

Compact Electrical Power Systems (ICEPS2)

The ISISPACE second generation Compact Electrical Power Systems (ICEPS2) are reliable, off-the-shelf EPS solutions for nanosatellite and CubeSat missions up to 3UXL.

price on requestdatasheet

Innovative Space Logistics

Modular Electrical Power System (IMEPS2)

The IMEPS2 is a second-generation modular electrical power system designed for small satellites, offering adaptable power solutions with superior efficiency and scalable redundancy

Flight Heritage	since 2020
Battery Packs	Up to 45Wh per PBP, stackable for redundancy

price on requestdatasheet

Innovative Space Logistics

Small Satellite Solar Panels

ISISPACE offers customizable small satellite solar panels designed for mission-specific needs, supporting 1U to 16U satellites.

price on request

US lunar lander company that became the first private company to land on the Moon (IM-1 Nova-C, Feb 2024), under NASA's CLPS lunar delivery program.

Intuitive Machines

Power & Propulsion Element (PPE)

The Power and Propulsion Element (PPE) is a high-power, solar electric propulsion spacecraft element built on the IM-1300 platform. Initially designed for NASA’s Gateway luna

price on request

CubeSat deployers, antennas, EPS and small-satellite systems.

ISISPACE Group

Compact Electrical Power System 2

Compact GaN-FET EPS for up to 3UXL CubeSats in 3 variants, with MPPT, battery heating, and 22.5–45 Wh energy storage.

Mass — Type A	184 ± 5 g
Mass — Type B	310 ± 5 g
Mass — Type C	360 ± 5 g
Volume — Type A	96 x 92 x 26.45 mm (PCB and top battery)
Volume — Type B	96 x 92 x 11.34 mm (PCB only)

price on requestdatasheet

ISISPACE Group

ISIS Modular Electrical Power Subsystem version 2 (v2)

The ISIS Modular Electrical Power Subsystem (IMEPSv2) is a second-generation, flexible EPS designed for larger nano-satellites and microsatellites from 3U upwards, offering improve

Manufacturer

ISISPACE

price on requestdatasheet

ISISPACE Group

ISISPACE Compact Electrical Power System

The ISISPACE Compact Electrical Power System (CEPS) is a second-generation compact power system for nanosatellites, ideal for 1U to 3U CubeSats, featuring GaN-FETs for improved sol

Form Factor	Compact single PC/104 form factor board solution
MCUs	FRAM based MCUs for improved radiation tolerance
Protection	Hardware voltage, over-current protection
MPPT	Hardware-based maximum power point tracking
Power Consumption	Designed for low (idle) power consumption

price on requestdatasheet

ISISPACE Group

Modular Electrical Power System 2

Second-generation modular EPS for 3U+ CubeSats, with distributed architecture, 45 Wh per battery pack, and 12 configurable output channels.

Mass — PCU	58 g
Mass — PBP	252.0 g
Mass — PBU	48.7 g
Mass — PDU	58 g (incl. Full CSKB)
Volume — PBP	90 x 96 x 21 mm

price on requestdatasheet

ISISPACE Group

Satellite Solar Panels

High-efficiency GaAs triple-junction CubeSat solar panels for 1U–12U missions, with integrated sun and temperature sensors.

Mass — 1U	50 g
Mass — 2U	100 g
Mass — 3U(XL)	150 g
Mass — 6U(XL)	300 g
Mass — 8U	400 g

price on request

Bengaluru-based space startup offering end-to-end CubeSat design, manufacturing, subsystem development, and ground station services for nanosatellite missions.

ISpaceI Satellite and Research

ISpaceI EPS — Electrical Power System

Integrated electrical power system for 1U–3U CubeSats with solar charging and regulated power distribution.

Compatible form factors	1U, 2U, 3U CubeSat
Power generation	Solar panels (body-mounted or deployable)
Energy storage	Onboard battery pack
Output	Regulated multi-voltage bus for subsystem distribution
Integration	Compatible with ISpaceI OBC and ADCS

price on request

Russian satellite manufacturer in Zheleznogorsk, Siberia; GLONASS-K/M navigation, Express GEO comms, Luch data relay, and Yamal satellites; 1,400+ spacecraft built.

ISS Reshetnev

Solar array drive assembly components

This product page describes solar array drive mechanical units designed for the Express-2000 and Express-1000 satellite platforms and their variants.

price on request

Developer of the IVO Quantum Drive, a pure electric propulsion technology, and CBAT wireless power transmission technology.

IVO Limited (Infinity Voltaic Orbits) is a US-based space propulsion company developing the Ionic Field Drive (IFD) — an electrically-powered thruster technology that the company claims generates thrust without propellant by manipulating el

IVO Limited

CBAT — Capacitive Based Aerial Transmission

Next-generation wireless power transfer technology transmitting electrical energy through air, walls, and water without physical contact or alignment.

Transfer medium	Air, walls, water, and other non-conductive materials
Alignment requirement	None — no pad or port alignment needed
Multi-device support	Single transmitter powers multiple devices simultaneously
Technology basis	Capacitive field coupling
Inventor	Richard Mansell (CTO, IVO Limited)

price on request

South Korean nanosatellite manufacturer offering CubeSat platforms, optical imagers, star trackers, solar panels, EPS, structures, and deployers for the commercial small satellite market.

Kairo Space

KSEPS Electrical Power System

CubeSat electrical power system with MPPT solar charging, battery management, and regulated power distribution.

Solar Charging	MPPT
Interface	PC/104 stack
Compatible Panels	KSSP series
Platform	1U–8U CubeSat

price on request

Kairo Space

KSSP Solar Panels

Body-mounted and deployable solar panels for CubeSat electrical power generation in LEO.

Types	Body-mounted and deployable
Cell Technology	Triple-junction
Compatible EPS	KSEPS
Form Factors	1U–8U CubeSat

price on request

Kayser Space designs, manufactures, integrates, and tests hardware and platforms for space programs, supporting over 100 missions and microgravity research.

Kayser Space

PPS mk1

The PPS mk1 is an autonomous space-qualified power distribution unit designed to convert and distribute 28 Vdc to multiple subsystems and payloads, integrating high-efficiency conv

Input Voltage	28 Vdc
Flight Heritage	ISS Columbus Module and multiple ESA programs

price on request

Kayser Space

PPS Power Distribution Units

Autonomous space-qualified power distribution units converting and distributing 28Vdc power — proven heritage on the ISS Columbus Module and multiple ESA programs.

Input/output voltage	28 Vdc (PPS mk1/mk2, VMU PCU)
ACLS AFP output	Non-isolated 120 Vdc
Flight heritage	ISS Columbus Module, multiple ESA programs

price on request

US energy and thermal management technology company delivering high-performance battery systems and thermal solutions for aerospace, defense, AI, robotics, and space applications.

KULR Technology

KULR ONE Space (K1S) Battery System

Flight-ready lithium-ion battery systems for spacecraft, CubeSats, and orbital vehicles — 100Wh to 400Wh series, passive propagation-resistant safety architecture, NASA WI-37A scre

Energy configurations	100 Wh, 200 Wh, 300-LT, 400 Wh series
Cell qualification	NASA WI-37A screened lithium-ion cells
Safety architecture	Passive propagation resistance (flame-arresting)
Housing	Anodized-aluminum, space-rated connectors
Variants	K1S-REACH, K1S-Forerunner (NASA 20793 PPR-qualified), K1S-SPARTAN (radiation-hardened)

price on request

KULR Technology

KULR Thermal Runaway Shield for Space

KULR Technology's carbon fiber thermal runaway shield protecting satellite battery packs — NASA Orion program-qualified containment system preventing cell-to-cell thermal propagati

Product	Thermal Runaway Shield (TRS) — cell-to-cell propagation containment
Material	Carbon fiber composite — absorbs and redirects thermal runaway energy
Flight Heritage	NASA Orion MPCV (crew vehicle) program qualification
Also	Thermal interface materials (TIMs), phase-change energy storage
NYSE	KULR (publicly listed)

price on request

Lanzo Batteries designs and manufactures lithium-ion battery packs for space energy storage, serving large satellites, small satellites, and CubeSats.

Lanzo Batteries

High Energy Space Battery Cells

Lanzo Batteries' high-energy lithium-ion battery cells and pack assemblies for satellite power storage — targeting higher specific energy and cycle life for small satellite constel

Product	Li-ion battery cells and pack assemblies for space (small satellites)
Target Energy	>200–250 Wh/kg specific energy (vs. 100–150 Wh/kg heritage space cells)
Includes	Cell monitoring electronics, protection circuits, structural housing
Market	Small satellite constellation operators (volume buyers)
Qualification	Radiation tolerance, vibration, cycle life testing for satellite mission assurance

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

Max Joule Tech develops high-energy battery systems for space exploration, Arctic expeditions, and unmanned aerial vehicles.

Max Joule

Arctic

Battery system engineered to reliably operate in extreme cold for Arctic expeditions.

price on request

Max Joule

Phoenix

Lightweight, high-energy battery system for unmanned aerial vehicles.

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

CubeSat Electrical Power System 1.0 (EPS)

CubeSat EPS with integrated BMS, 4 MPPT converters, 18 output channels, up to 175 W output power, and optional 161 Wh external battery pack.

MPPT converters	4 converters with 8 solar panel input channels
Solar panel input voltage	Wide range (multiple MPPT channels)
Output power (max)	175 W
Output channels	18 channels (switchable autonomously or by ground command)
Battery type	On-board Lithium-Ion

from €8 470

NanoAvionics

CubeSat GaAs Solar Panel

NanoAvionics GaAs (Triple junction GaInP/GaInAs/Ge epitaxial structure) solar arrays are high-performance, space-grade solar cells designed for CubeSat missions with high power req

Solar cell efficiency

up to 29.5 %

price on request

NanoAvionics

SmallSat EPS 2.0

Electrical Power System 2.0 for small-satellite and microsatellite platforms.

Type	SmallSat Electrical Power System
Class	Microsatellite / SmallSat
Flight heritage	60+ satellites launched, 300+ in production (per nanoavionics.com)

price on request

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

NBSpace

CubeSat Electrical Power System (EPS)

Complete CubeSat EPS for 1U, 3U, and 6U missions — includes Battery Pack Unit, MPPT solar charge controller, and PCDU for reliable power throughout the mission.

Components	Battery Pack Unit (BPU), MPPT controller, PCDU
Supported form factors	1U, 3U, 6U CubeSat
Test equipment	Solar array simulator
Key features	Scalable power budget, high-efficiency, space-grade

price on request

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

NPC Spacemind

D-SP Deployable Solar Panels

Deployable solar panel wings for 3U-16U CubeSats, vertical and lateral (single/double wing) configurations.

D-SP3X-V	3U/6U vertical deployment, Peak power 8-8.8 W, Voc 18.2-19.3 V
D-SP3X-L-1W	3U/6U lateral, single wing
D-SP3X-L-2W	3U/6U lateral, double wing
D-SP6X-V	6U-class vertical deployment
D-SP6X-L-1W	6U-class lateral, single wing

price on request

NPC Spacemind

D-SP6X-L-1W

The D-SP6X-L-1W is a deployable solar panel with a single wing lateral configuration, compatible with 6U/12U CubeSat structures, offering high-efficiency triple junction solar cell

Deployable Solar panel for	XY side
Configuration	1 Wing Lateral
Compatibility	6U/12U CubeSat structures
Solar cells	High efficiency triple junction UTJ
Peak power	18.4 - 20 W

price on request

NPC Spacemind

GEMINI EPS

Modular Electrical Power System for 3U to 16U CubeSat platforms, supporting up to 8 parallel battery packs and multiple programmable output voltages.

Platform Compatibility	3U - 16U Cubesat platforms
Input Channels	6 Input channel - voltage per channel 5 to 20V
Battery Packs	Up to 8 parallel battery packs
Battery Pack Capacity	84 Wh for 8 cells (per unit)
Output Bus	Programmable Output Bus 3.3V-5V-6/12V-24V

price on request

NPC Spacemind

SP Body-Mounted Solar Panels

Body-mounted solar panel family for 1U-16U CubeSats, X/Y and Z variants, with integrated sensors.

SP1X	1U side, Mass 40 g, Peak Power 2.3-2.5 W, Voc 5.2-5.5 V
SP1Z	1U zenith panel variant
SP2X	2U side panel
SP2Z	2U zenith panel variant
SP3X	3U side panel

price on request

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

U.S. manufacturer of deployable spacecraft structures and subsystems - booms, solar arrays and RF antennas - built on proprietary high-strain composite and origami-inspired technology.

Opterus Research and Development

Modular Self Stiffening Array (MOSSA)

The MOSSA is a modular, panel-based solar array for SmallSats, designed for missions requiring high precision pointing or rapid slewing, offering configurations from 1 to 9 panels.

price on requestdatasheet

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.

External Power Supply

A desktop switching power supply, available in +5Vdc or 6-12Vdc output variants, used to bench-power Pumpkin's Development Board and Motherboard Module during ground development.

Price	$80.00
Output voltage options	5Vdc; 6-12Vdc
Connector	5.5/2.1mm barrel plug
AC input cord	IEC power cord receptacle; 3-prong / grounded IEC cord provided (USA customers)
Compatible with (5Vdc supply)	Motherboard Module (MBM); Motherboard Module 2 (MBM 2); Development Board (DB)

$80

Pumpkin, Inc.

High-Power Electrical Power System Module (EPSM1)

Multi-channel space-grade EPS module with 6 MPPT solar inputs (max 480W total), dual Li-Ion battery ports, and configurable 3.3–28V output rails with >99% efficiency.

Solar Input Channels	6
Max Total Solar Input	480 W
MPPT Frequency	250 kHz
Max Input per Channel	4 A at 28 V
Battery Ports	2

$48 000datasheet

Pumpkin, Inc.

High-power Multi-channel Electrical Power System Module (EPSM1)

A high-performance, highly efficient FPGA-driven, GaNFET-based multichannel power system module for small satellites, handling up to 480W of solar input and ~300W of regulated outp

Switching blocks	Twelve non-isolated 250 kHz switching blocks
Solar array inputs (SAI1-SAI6) max total power	480 W
Battery reserve power	up to 112 W per battery
Battery charge voltage	16.8 V Li-Ion, CC/CV, up to 6 A
Output 3V3 / 5V0 current	up to 5 A each

$48 000

Pumpkin, Inc.

Intelligent Lithium Battery Module (BM2)

Space-grade 8-cell Li-Ion battery module with coulomb-counting SoC, cell balancing, configurable voltage (2S4P/3S2P/4S2P), and 15A max output — up to 100Wh.

Cell Type	8× 18650-size Li-Ion
Configuration Options	2S4P (8.4V), 3S2P (12.6V), 4S2P (16.8V)
Capacity Options	72 Wh / 86 Wh / 100 Wh
Max Continuous Output	15 A
Peak Output Power	160 W

$10 500datasheet

Pumpkin, Inc.

Intelligent Protected Lithium Battery Module with SoC Reporting (BM2)

Pumpkin's flight-qualified, protected lithium-ion battery module (BM2) with state-of-charge reporting, configurable cell topology and capacity, for CubeSats and small satellites.

Battery configuration option 2S4P	8 cells, 5.2-8.4V
Battery configuration option 3S2P	6 cells, 7.8-12.6V
Battery configuration option 4S2P	8 cells, 10.4-16.8V
Cell capacity option 1	2500mAh (72Wh with 8 cells)
Cell capacity option 2	3000mAh (86Wh with 8 cells)

$10 500 – $12 500datasheet

Pumpkin, Inc.

Linear EPS Module (LEPSM1)

A low-cost development-only Electrical Power System module with 10-20Wh of battery energy that supplies +7.4Vdc, +5Vdc and +3.3Vdc rails to a CubeSat Kit stack during bench develop

Price range	$980.00 - $1,145.00
Classification	Development Hardware | Not for Space Use
Battery energy	10 Wh (standard battery) or 20 Wh (double battery)
Output rails	+7.4Vdc (nominal), +5Vdc, +3.3Vdc
Battery voltage (VBATT)	6-8.4 Vdc (2S Lithium Polymer)

$980 – $1 145datasheet

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

Roll Out Solar Array (ROSA)

Redwire's Roll Out Solar Array (ROSA) is a scalable, high-power solar solution featuring a unique rollable stowage configuration for compact volume and mass optimization.

Configuration	Diamond
Deployed Length (m)	8.6
Mass (kg)	36
BOL Power (kW)	3.3
Stowed Width (m)	2.32

price on requestdatasheet

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

French space company developing ultra-high-power orbital solar platforms and AI-enabled robotic systems for in-space assembly, maintenance, and power generation.

Rovial Space

Rovial Breakthrough™ Solar Space Platform

Ultra-high-power orbital solar platform delivering 100 kW to 500 kW for commercial and defence space applications with a 15-year design life.

Power Output	100 kW to 500 kW
Operational Lifespan	15 years
Deployment	Full platform capability achievable in a single launch
Target Applications	High-power communications, in-space data centres, space lasers, lunar power, power beaming

price on request

Saft is a world-leading manufacturer of advanced technology batteries for space, defence, aviation, and industrial applications.

Saft

4S1P VES16 Battery

Compact 64 Wh / 4.5 Ah space lithium-ion battery for microsatellites and nanosatellites in LEO and small GEO orbits.

Chemistry	Li-ion
Cell Configuration	4S1P
Capacity	4.5 Ah
Nominal Energy	64 Wh
Pack Voltage Range	13.2 – 16.4 V

price on request

Saft

MP & VL Batteries for Launchers

Launcher-qualified prismatic MP and cylindrical VL rechargeable lithium-ion batteries for space launch vehicles.

Chemistry	Li-ion
Cell Formats	Prismatic (MP), Cylindrical (VL)
VL Power Variants	Power (P), Very High Power (U)
Charge Temperature Range	-20 to +60°C
Discharge Temperature Range	-50 to +60°C

price on request

Saft

VES16 11S16P Battery

High-capacity 11,264 Wh / 288 Ah space lithium-ion battery for large satellite platforms.

Chemistry	Li-ion
Cell Configuration	11S16P
Capacity	288 Ah
Nominal Energy	11,264 Wh
Pack Voltage Range	29.7 – 45.1 V

price on request

Saft

VES16 8S4P Battery

512 Wh / 18 Ah space lithium-ion battery in 8-series 4-parallel configuration for LEO and small GEO satellites.

Chemistry	Li-ion
Cell Configuration	8S4P
Capacity	18 Ah
Nominal Energy	512 Wh
Pack Voltage Range	25.0 – 32.8 V

price on request

Saft

VES16 Cell

Space-qualified D-size 16 Wh lithium-ion cell designed for LEO and GEO satellite applications.

Chemistry	Li-ion NCA
Nominal Capacity	4.5 Ah
Nominal Energy	16 Wh
Specific Energy	> 155 Wh/kg
Voltage Range	2.7 – 4.1 V

price on request

Saft

VL51ES Li-Ion Battery for GEO and MEO

High-power space battery based on Saft VL51ES Li-ion cells, specifically designed for GEO and MEO spacecraft applications requiring sustained high discharge rates.

Cell type	VL51ES Li-ion cylindrical cell
Application	GEO and MEO spacecraft
Performance type	High power
Mission profile	Up to 72-min eclipses at GEO; MEO radiation environment
Design lifetime	> 15 years (GEO class)

price on request

SkyLabs is a Slovenian space-technology company that designs and manufactures miniaturized, fault-tolerant on-board data handling, communications, power, ADCS/GNC and EGSE equipment for small satellites.

SkyLabs d.o.o.

NANOeps

Highly integrated electrical power system with battery management and power control/distribution module.

Standard	ISO 19683, IPC Class 3+
TRL	9
MAIT	In-house
Battery pack capacity	Up to 172 Wh (multiple units in parallel configuration)
Battery pack life time	> 30000 re-charge cycles @ 20% DoD (80% EOL capacity)

price on request

SkyLabs d.o.o.

NANOeps-AMPPT

Safest and most accurate solar array energy conversion subsystem using analog maximum power point tracking.

Standard	ISO 19683, IPC Class 3+
TRL	9
MAIT	In-house
AMPPT channels	8 channels with dedicated AMPPT each
AMPPT efficiency	> 80% (at 25°C)

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

Solar MEMS Technologies is a Spanish company specializing in MEMS-based sun sensors and star trackers for satellite attitude determination systems.

Solar MEMS Technologies

nanoSSOC-D60 Digital Sun Sensor

High-accuracy digital fine sun sensor for nanosatellites, providing two-axis sun vector measurement with MEMS technology and SPI/UART interface.

Field of View	120° x 120° (±60° each axis)
Accuracy	< 0.5° (1σ)
Interface	SPI / UART
Mass	< 5 g
Power	< 100 mW

price on request

La Mirada, CA manufacturer of JANS-certified high-power semiconductors and power electronics for aerospace, defence, and space applications since 1967, with heritage on NASA Artemis.

Solid State Devices Inc

SFC85N90S2 SiC Power MOSFET

85 A, 900 V, 17 mΩ max hermetically sealed SiC N-channel power MOSFET with 100 kRad total dose tolerance. Radiation-tolerant drop-in replacement for silicon MOSFETs.

Drain-source voltage (Vdss)	900 V
Continuous drain current (Id)	85 A
On-resistance (Rds_on) typical	10 mΩ
On-resistance (Rds_on) maximum	17 mΩ
Power dissipation (Pd)	288 W

price on request

Solid State Devices Inc

SFH06055-20 High Side Power Switch

20 A, 60 V, 55 mΩ radiation-tolerant hermetic high-side power switch in LCC20 ceramic surface-mount package with logic-level input.

Continuous drain current (Id)	20 A
Drain-source voltage (Vdss)	60 V
On-resistance (Rds_on)	55 mΩ
Input	Logic level input voltage
Protection	Zener-protected gate, radiation tolerant

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

Small Solar Arrays

Rigid bodymount and deployable solar arrays for small satellites, tested beyond GEVS, fault-tolerant to micrometeorites and shading.

Configurations	Bodymount, Rigid Deployable
Materials	Space stable (UV, radiation, atomic oxygen hardened)
Fault tolerance	Micrometeorite and localised shading tolerant
Testing	Tested beyond GEVS
Stiffness	High deployed stiffness for high pointing capability

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

Ukrainian (Dnipro) manufacturer of Hall-effect electric propulsion systems for satellites: thrusters, power processing units, and xenon feed systems, with flight heritage since 2023.

Space Electric Thruster Systems (SETS)

PPU-200 (Power Processing Unit)

The PPU-200 is a power management unit for LEO satellites, designed to supply Hall-effect thrusters in the 80–230 W range and control the Xenon Feed System.

Power range for Hall-effect thrusters	80–230 W
Flight heritage	Yes
Anode power supply architecture	Patented

price on requestdatasheet

Space Electric Thruster Systems (SETS)

PPU-500 (Power Processing Unit)

The PPU-500 is a power processing unit designed for 500 W class electric propulsion systems, providing efficient and reliable power management for Hall-effect thrusters.

Anode power	Up to 500 W
Input voltage	24-36 V
Operating temperature	-35 to +80 C
Efficiency	Up to 94%

price on requestdatasheet

Aerospace engineering company providing modular small satellite bus platforms (Chameleon), avionics, and range instrumentation systems for defense and commercial space missions.

Space Information Laboratories (SIL)

Intelli-Pack

Intelli-Pack is a dependable, high energy density, rapidly rechargeable lithium-ion battery technology for launch vehicles, small satellites and UAS/RPA.

Configurations	6U, 12U, 27U
Attitude accuracy	<0.1 degree nadir pointing
GPS	L1/L2 high dynamic receiver
Power (6U)	45W average on-orbit
Power (27U)	90W average on-orbit

price on request

Space Inventor ApS is a Danish second-generation NewSpace company providing non-ITAR CubeSat, nanosat, and microsat components, platforms, and turnkey satellite missions with full vertical integration, headquartered in Aalborg with offices

Space Inventor ApS

BAT module

The BAT module is a Lithium-Ion battery available in 4-cell (14.4V) and 8-cell (28.8V) versions, designed for extended lifetime and easy integration in CubeSats and microsatellites

Nominal Voltage (4-cell variant)	14.4 V
Nominal Voltage (8-cell variant)	28.8 V
Technology	Lithium-Ion
Capacity (single module)	100 Wh

price on request

Space Inventor ApS

Modular Power Platform (MPP)

Scalable power architecture built on P4-series equipment, supporting solar array power from a few hundred watts up to 4 kW.

MPP-700-6U solar array power	110 W
MPP-700-6U battery energy storage	204 Wh
MPP-700-6U max combined load power	408 W
MPP-700-16U solar array power	220 W
MPP-700-16U battery energy storage	204 Wh

price on request

Space Inventor ApS

MPPT

A 4-channel Maximum Power Point Tracker that connects satellite solar panels directly to the spacecraft battery bus, optimizing solar array power conversion for battery charging.

MSRP	€7,000
PV input channels	4
Output	Two output power buses via ideal diode combination
Redundancy	Dual MCUs, CAN interface

price on request

Space Inventor ApS

Power Distribution Unit

A Power Distribution Unit (PDU) available in four variants with three different voltage output levels, featuring redundant MCUs, CAN interface, and current sensing on all 8 outputs

MSRP

€7.000

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.

Amun

Amun is a reliable power management unit for small satellites, designed in the PC/104 form factor for 0.5U–2U CubeSats.

Operating temperature	-40°C to +85°C
Dimensions	95.9 x 90.2 x 19.7 mm (0.2U)
Mass	185 g
Power outputs	1x fixed 3.3 V
Power outputs	1x fixed 5 V

price on requestdatasheet

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

Space Solar Panels

Fully assembled space solar panels built to customer specifications, integrating Spectrolab's multijunction solar cells for maximum EOL performance across all orbital environments.

Integration	Multijunction solar circuits bonded to customer-furnished substrate
Optimization	Engineered for maximum EOL performance per mission profile
Cell Technology	XTE or XTJ family multijunction cells
Flight Heritage	500+ spacecraft powered by Spectrolab panels

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

SPUTNIX

High-power distribution and control unit

A power switching unit (PSU-h) distributing main/backup power lines and redundant data/timing buses between up to 8 onboard devices.

Dimensions, mm	244 x 171 x 45 (without fasteners)
Mass, kg	1.1
Power voltage, V	22-34
Power consumption, Wt	5
Duplicated interfaces	CAN2B

price on request

SPUTNIX

Power supply system (with battery unit)

A two-module CubeSat EPS (SXC-PSS-03) consisting of a power system controller (SXC-PSU-03) and battery module (SXC-BAT-03) for solar power collection, storage, and distribution.

SXC-PSU-03 Dimensions	98.4 x 96 x 19 mm (±0.2mm)
SXC-PSU-03 Mass	20 ± 2 g
Solar panels channels	3
Solar panel type	GaAs, Si
Solar panel voltage	3.5..5.5V

price on request

SPUTNIX

Regulation and control equipment

The EPS regulation and control equipment (RCE) that manages battery charging/discharging and power distribution together with solar and storage batteries.

Dimensions, mm	306 x 161 x 140 (without fasteners)
Mass, kg	7
Power voltage, V	22-34
Power consumption, Wt	10
Duplicated interfaces	CAN2B, RS485, SpaceWire

price on request