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
Peak Power	2.45 W
OC Voltage	5.2 V

price on requestdatasheet

2NDSpace Srl

CORE-01 1U Cubesat Solar panel

The CORE-01 is a 1U CubeSat solar panel designed for reliable power generation in space, featuring dual redundant protection and customizable integration options.

Peak Power	2.45 W
OC Voltage options	5.2 V
Suggested for	1U
Side	Lateral
Form Factor	1U Lateral XY

price on requestdatasheet

2NDSpace Srl

CORE-01Z 1U Cubesat Top Solar panel

The CORE-01Z is a 1U CubeSat top solar panel from 2NDSpace Srl, offering 2.45 W peak power and proven reliability for small satellite missions.

Peak Power	2.45 W
OC Voltage options	5.2 V
Suggested for	1U
Side	Top/Bottom
Form Factor	1U Z

price on requestdatasheet

2NDSpace Srl

CORE-02 2U Cubesat Solar panel

The CORE-02 is a 2U CubeSat solar panel designed for lateral mounting, offering 5W peak power and dual redundant protection.

Peak Power	5 W
OC Voltage options	5.2 V
Suggested for	2U
Side	Lateral
Form Factor	2U Lateral XY

price on requestdatasheet

2NDSpace Srl

CORE-03 3U Cubesat Solar panel

The CORE-03 is a 3U CubeSat solar panel from 2NDSpace Srl, offering reliable power generation with options for various open-circuit voltages and a robust design suitable for 3U and

Peak Power	8.54 W
OC Voltage options	5.2 / 7.8 / 16.4 V
Suggested for	3U / 6U
Side	Lateral
Form Factor	3U Lateral XY

price on requestdatasheet

2NDSpace Srl

CORE-06Z 6U/8U Cubesat Top Solar panel

The CORE-06Z is a top solar panel designed for 6U/8U CubeSats, offering 4.9 W peak power and dual redundant protection.

Peak Power	4.9 W
OC Voltage options	5.2/10.4 V
Suggested for	6U/8U
Side	Top/Bottom
Form Factor	2x1

price on requestdatasheet

2NDSpace Srl

CORE-08 4U/8U Cubesat Solar panel

The CORE-08 is a lateral solar panel designed for 4U/8U CubeSats, offering a peak power of 11W and multiple open-circuit voltage options.

Peak Power	11 W
OC Voltage options	5.2/7.8/10.4/ 23.4 V
Suggested for	4U/8U
Side	Lateral
Form Factor	1x4

price on requestdatasheet

2NDSpace Srl

CORE-12 6U/12U Cubesat Solar panel

The CORE-12 is a solar panel designed for 6U/12U CubeSats, offering proven performance in space with redundant power lines and ECSS compliance.

Peak Power	19.6 W
OC Voltage options	10.4/20.8 V
Suggested for	6U/12U
Side	Lateral
Form Factor	2x3

price on requestdatasheet

2NDSpace Srl

CORE-12Z

The CORE-12Z is a 12U/16U CubeSat top solar panel, offering reliable power generation with a peak power of 9.76 W and multiple voltage options.

Peak Power	9.76 W
OC Voltage options	5.2/10.4/ 20.8 V
Suggested for	12U/16U
Side	Top/Bottom
Form Factor	4x4

price on requestdatasheet

2NDSpace Srl

CORE-16

The CORE-16 is an 8U/16U CubeSat solar panel designed for reliability and easy integration, offering multiple voltage options and customizable layouts.

Peak Power	24.4 W
OC Voltage options	10.4/13.0/ 26.0 V
Suggested for	8U/16U
Side	Lateral
Form Factor	2x4

price on requestdatasheet

2NDSpace Srl

DROP Deployable Solar Panels

2NDSpace's DROP deployable solar panels offer a modular design with dual, triple, or multi-wing configurations and the option for solar cells on both sides, maximizing surface area

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	7.5 W
Backstring option	+7.5 W
Body mounted option	+7.5 W

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	+10 W
Body mounted option	+10 W

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	+20 W
Body mounted option	+20 W

price on requestdatasheet

2NDSpace Srl

DROP-16 8U/16U Deployable Solar panel

The DROP-16 is a deployable solar panel system designed for 8U/16U CubeSats, offering customizable power configurations and a dual redundant deployment system.

Suggested for	8U/16U
Deployment System	Dual redundant
Deployment Configuration	135°/90°
OC Voltage	24.3 V
N° of deployable Elements	1

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

2NDSpace Srl

SOLO-EPS-4

The SOLO-EPS-4 is a Cubesat Power Distribution and Control Unit (PDCU) and Battery Pack designed for 1U to 27U platforms, offering controllable power outputs and multiple MPPT inpu

Controllable power outputs	12x
Controlled voltage outputs	3.3 V / 5.0 V / 12 V / 16 V
MPPT Inputs	6x
Peak Power	100 W
Energy Storage	52 WHr

price on requestdatasheet

2NDSpace Srl

SOLO-EPS-8

The SOLO-EPS-8 is a Cubesat Power Distribution and Control Unit (PDCU) and Battery Pack designed for 1U to 27U platforms, offering controllable power outputs and integrated energy

Controllable power outputs	12x
Controlled voltage outputs	3.3 V / 5.0 V / 12 V / 16 V
MPPT Inputs	6x
Peak Power	160 W
Energy Storage	100 WHr

price on requestdatasheet

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	0.8 V to 5.5 V
Maximum current	2 A
Switch-off time	10 μs maximum
Operating temperature	-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	1.6 V to 2.8 V
3dpm0237 output current	±1 A
3dpm0237 package	SOP24
3dpm0318 (ddr2) input voltage	1.6 V to 2.8 V
3dpm0318 output current	±1 A

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	5 V ±10%
3dpm0211 output voltage	1.225 V to 3.8 V (adjustable)
3dpm0211 package	14-pin Gull Wing SMD
3dpm0289 input voltage	4.5 V to 12 V
3dpm0289 output voltage	1 V to 5 V (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	3 V to 12 V
Maximum line current	7 A
Voltage drop	90 mV at 7 A
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	3.3 V; 5 V; and 12 V
Latching current limit (LCL)	10 Configurable
Interfaces	I2C
Max. battery voltage	8.2 V

price on requestdatasheet

AAC 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	+3.3 V, +5 V, +12 V regulated rails
Battery temp range	-20°C to +60°C (space-qualified)
Design life	3–5 year design lifetime
Flight heritage	Hundreds of CubeSat missions (NASA, ESA, Planet, Spire, JAXA, others)

price on request

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 9 W per 3U populated face
Operating temperature range	-40°C to +80°C
Photon-dd - 3u size only stowed height	9.55 mm

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 requestdatasheet

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	8.2 V
Regulated power buses	3.3 V, 5 V, 12 V
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 100 V
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 100 V 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 23 kW at 100 V
Flight heritage	Alphabus, E3000, E3000-NEO, Galileo; legacy from PSR 50 V with more than 80 units in fligh
Mass	2.5 kg
Dimensions	395 x 125 x 65 mm3
Lifetime	10 years in LEO

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.

Design life	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)
Mass	10 kg

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 temperature	-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 150 W
Output voltage	up to 22 V
Lifetime	minimum 2 years in LEO
Data connector	8-pin Hirose 1.25 mm

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

Argotec Srl

ELEKTRA BATTERY PACK

Scalable Li-ion Battery Pack with Integrated Battery Management System (BMS) optimized for peak performance in Deep Space and LEO.

price on request

Argotec Srl

ZEUS PCDU

ZEUS (Zenith Energy Utilization System) is a Modular Power Conversion & Distribution Unit designed to power a wide range of microsatellite platforms.

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
Supply 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
Supply 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

AstroForge is a deep-space mining company that builds spacecraft to track and extract valuable metals from asteroids, aiming to integrate space resources into Earth's supply chain.

AstroForge

Spacecraft Solar Array Structures

AstroForge designs and engineers solar array structures for spacecraft, balancing power generation, structural integrity, mass limitations, and deployment reliability.

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.

Supply voltage	23.1 V (customizable)
Capacity	7.5 Ah (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 23.1 V (customizable)
Battery interface	6x 23.1 V (customizable)
Supply voltage	23.1 V (customizable)
Regulated voltages	12 V, 5 V, 3.3 V (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 Array Drive Assemblies

Blue Canyon Technologies' high-performance, lightweight, and modular SADA design maximizes payload operation time through a rotary interface between a spacecraft and its solar pane

SADA-3 Mass	1.5 kg
SADA-3 Volume	12.5 cm x 11.1 diameter
SADA-3 Rated Torque	10 Nm
SADA-3HP Mass	1.66 kg
SADA-3HP Volume	15.0 cm x 11.1 diameter

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	5 V, 12 V, Unregulated 28 V
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 space applications.

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

Power VPX

800, 1000W Power Module in VPX form factor

Form factor	3U VPX power module per VITA 62.0 / VITA 48.2, 2.00 inch pitch
Envelope (max)	3.94 in W × 6.63 in L × 2.00 in H
Mass	3.6 lb typical, 3.8 lb maximum
Cooling	Conduction cooled through card edge and wedge-lock path
Operating temperature	−40 °C to +85 °C card-edge

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

Comat's Solar Array Drive Mechanisms (SADM) ensure precise and continuous solar array orientation toward the Sun, maximizing spacecraft power generation throughout the mission.

SADM-CP Power Transfer	Up to 400 W per wing
SADM-CP Maximum Torque	0.35 Nm
SADM-CP Operational lifetime	Minimum 5 years in LEO
SADM-HP Power Transfer	Up to 4000 W per wing
SADM-HP Maximum Torque	0.35 Nm

price on requestdatasheet

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)	200 W at 28 V
Power (transfer capability)	400 W at 50 V
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 (2)	DP-ATE-8219
Description (2)	ATS Power Module
Product name (3)	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.

Power

up to 400 W

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 2 kW

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)	500 W to 5 kW
Solar cell technology	Cell Agnostic: ELSA can support III-V and Silicon technologies
Stowed first mode	>40 Hz standard
Deployed first mode	>.25 Hz 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 requestdatasheet

Dhruva Space is an Indian space technology company founded in 2012, providing satellites, Earth stations, and launch services as integrated or individual solutions.

Dhruva Space

Solis & Solis+ Spacecraft Solar Arrays

Solis and Solis+ are Spacecraft Solar Arrays developed by Dhruva Space, optimised for reliability in Space, supporting satellites and spacecraft of various sizes with power capacit

Compatibility (Solis)	0.5U, 1U, 3U, 6U, 12U, 16U CubeSat platforms
Power (Solis 1U)	2.4 W
Power (Solis 3U)	8.4 W
Power (Solis 6U)	4.8 W
Power (Solis 12U)	16.8 W

price on requestdatasheet

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

COTS Solar Arrays for Satellites

DHV Technology offers commercial off-the-shelf solar array solutions for satellites, providing ready-to-market qualified products to reduce engineering costs and project timelines.

price on request

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 900 W
Pcdu battery module capacity	415 Wh ~ 1660 Wh
Nanoeps CUBESAT compatibility	non-deployable 3U to triple deployable 2U, 3U or 6U
Nanoeps power bus generation	3.3 V, 5 V, 12 V 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

Standard and custom solar array solutions for CubeSat platforms ranging from 1U to 16U, with deployables and custom cut-out areas available.

Pmp (1U)	2.4 W
Vmp (1U)	4.8 V
Imp (1U)	0.5 A
Mass (1U)	< 50 g
Pmp (2U)	4.8 W

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

South African manufacturer of high-performance electro-optical imaging payloads and satellite platforms for Earth observation.

Dragonfly Aerospace

28-300 Battery Module

Dragonfly's flight-proven 28V LFP (Lithium Iron Phosphate) high-power, modular spacecraft energy storage solution, designed with ITAR-free, commercial off-the-shelf (COTS) componen

Topology	9s4p
Chemistry	LFP
Nominal voltage	29,7 V
Capacity	297 Wh
Discharge - continuous	20 A (600 W, 2C)

price on requestdatasheet

Dragonfly Aerospace

Electrical Power System

Dragonfly’s advanced 28V Electrical Power System designed for spacecraft power control and distribution, now in its 8th generation with heritage design for exceptional reliability

Total input, output & battery power	1500 W
Supply voltage	29.7 V (22 - 32 V)
Communication interfaces	CAN Telemetry & Telecommands, DCL (Direct Command Line) Telecommands
Operating temperature	-10 °C to +50 °C
Dimensions	211 x 153 x 175 mm

price on requestdatasheet

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	+7.4 V
Fully charged voltage per battery	+8.2 V
Fully charged current per battery	1 A
Maximum discharge current per battery	8 A

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 (2)	High sensitivity Silicon photodiode included.
Connectors	Three 4-pin solar array power output for flexible panels interconnection.
Connectors (2)	One 4-pin for temperature sensor.

price on requestdatasheet

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

EnduroSat

3U Deployable Solar Array

Deployable solar panels for CubeSats, offering high power output and radiation resistance with 29+% efficiency at End-of-Life.

Power efficiency at BOL	30+%
Power efficiency at EOL	29+%
Number of cells	14 (Single Deployable) or 21 (Double Deployable)
Max power in LEO	16.8 W (Single Deployable) or 25.2 W (Double Deployable)
Reverse bias protection	Internal bypass diode

price on request

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 W
Max voltage	17.5 V
Max current	512 mA

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

6U Solar Panel

The 6U CubeSat Solar Panel provides high power output and radiation resistance with over 29% efficiency at End-of-Life (EOL) for CubeSats.

Power efficiency at BOL	30+%
Power efficiency at EOL	29+%
Number of cells	16
Max power in LEO	19.2 W
Reverse bias protection	Internal bypass diode

price on request

EnduroSat

8U Deployable Solar Array

Deployable solar panels for CubeSats, offering high power output and radiation resistance with over 29% efficiency at End-of-Life.

Power efficiency at BOL	30+%
Power efficiency at EOL	29+%
Number of cells	40
Max power in LEO	48 W
Reverse bias protection	Internal bypass diode

price on request

EnduroSat

8U SOLAR PANEL

The EnduroSat 8U Solar Panel provides high power output and radiation resistance for CubeSats, featuring efficient solar cells and configurability.

Power efficiency at BOL	30+%
Power efficiency at EOL	29+%
Number of cells	20
Max power in LEO	24 W
Reverse bias protection	Internal bypass diode

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 Wh
System bus (vBatt)	30-50
Regulated power buses	12, 28 V
Max continuous current (28V)	125
Supply voltage	up to 70 V

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® 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 12 W solar sections per module, digital MPPT per channel
Det module	Up to 5x 20 W solar sections per module (Direct Energy Transfer)
Distribution module	Up to 10 W @5V and 6 W @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	2.5 W to 500 W
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

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

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 BP8 100 Wh

NanoPower BP8 100 Wh is a high-capacity lithium-ion battery pack engineered for space applications, offering reliable and efficient power storage for various space missions.

Nominal Wattage	100 Wh
Cell Type	18650 ion cells
Cell Capacity	3500 mAh (Nominal)
Nominal Voltage	28.8 V
Max Current Discharge	4 A

price on requestdatasheet

GomSpace

NanoPower BPX 100 Wh

The NanoPower BPX 100 Wh is a Lithium-ion battery pack with a built-in heater, designed for CubeSats to provide optimal power within a compact form factor.

Nominal Voltage	28.8 V
Nominal Wattage	100 Wh
Max Current Discharge	6 A
Dimensions	93 mm x 86 mm x 41 mm
Mass	Approximately 500 grams

price on requestdatasheet

GomSpace

NanoPower DSP

The Deployable Solar Panel System (DSP) is designed for 3U or 6U satellites, featuring three panels connected with spring-loaded hinges that deploy once in space.

Operational Temperature Range	-60°C to +80°C
Solar Panel Efficiency	30%
Power Output per Cell (LEO)	Up to 1.15 W
Effective Area per Solar Cell	30 cm²
Cell Base Material	GaInP/GaAs/Ge on Ge substrate

price on requestdatasheet

GomSpace

NanoPower MSP

The NanoPower MSP (Modular Solar Panel System) is a versatile and reliable solar panel system designed for GomSpace satellites and compatible with various CubeSat structures.

Operational Temperature Range	-55°C to 150°C
Internal Temperature Sensor Range	-40°C to +85°C
External Temperature Sensor Range	-55°C to +175°C
Solar Cell Variants	AzurSpace 3G30A and CESI CTJ-LC
Solar Cell Effective Area	30 cm²

price on requestdatasheet

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

GomSpace

NanoPower P60

The NanoPower P60 is an Electrical Power System (EPS) designed for nanosatellite missions, offering modularity and configurability to optimize power setups for unique mission requi

Max output power	Up to 128 W
Max current from batteries	4 A
Dimensions	92 mm x 88.9 mm x 19.9 to 28.9 mm
Mass	<80 g + nof ACU * 54 g + nof PDU * 47 g
P60 Dock modules supported	Up to 4 (Mix of ACU, PDU and one A3200)

price on requestdatasheet

GomSpace

NanoPower P80

The NanoPower P80 is an Electrical Power System (EPS) designed for power collection and distribution in satellites ranging from 6U to microsat sizes, capable of handling solar arra

Max Output Power	300 W
Solar Input Channels	12 MPPT 25 V
Output Converters	Up to 16
Output Channels	Up to 96
Input Channels	Up to 48

price on requestdatasheet

GomSpace

NanoPower TSP-45W

The NanoPower TSP-45W enhances satellite platform’s power efficiency through a deployable solar array equipped with sun tracking, seamlessly integrating with platforms as compact a

Cells per panel	15
Configuration	7S + 8S
Power production per cell	~1 W at 1367 W/m2 (BOL)
Total power production per array	~45 W
Communication	I2C protocol

price on requestdatasheet

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 (2)	Bonded assembly
Substrate manufacturing capabilities (3)	Autoclave cure
Substrate manufacturing capabilities (4)	Machining
Substrate manufacturing capabilities (5)	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

HEMERIA designs, produces, and supplies space systems, vehicles, and defense equipment for commercial, institutional, and scientific customers.

Hemeria

Emergency power supply

HEMERIA designs and manufactures emergency or back-up power supply systems such as uninterruptible power supply (UPS) to power critical systems in the event of main power grid fail

price on request

Hemeria

Power converters

HEMERIA designs and manufactures AC/DC, DC/DC and DC/AC converters, ensuring a high-quality power supply suited to the energy source of your on-board grid.

Converter solutions	1 to 500 kVA
Reliability and availability	High levels over several decades
Power density and output	High
EMC environments	Severe
Solutions	Customized and modular

price on requestdatasheet

Hemeria

Solar arrays

HEMERIA designs and builds solar arrays for all types of spacecraft, nano or micro satellites, rovers and transfer vehicles, offering a reliable and proven solution with controlled

Number of panels	1-3 panels per array
Range	From 30 W to 1 KW
Cells	Azurspace AZUR 3G30A / Spectrolab XTE CIC
Lifetime	From 5 to 8 years in orbit
Electrical I/F	Sub D connector

price on requestdatasheet

Hemeria

Variable speed drives

HEMERIA designs and manufactures variable speed drives to pilot motors and rotating machines in terms of speed and power, offering modular solutions with high reliability and guara

Drives and actuator range	1 kVA up to 100 kVA
Control logic	FPGA or DSP
Control type	Open-loop or closed-loop

price on request

Indian small satellite manufacturer offering flight-proven platforms, subsystems, and mission-as-a-service solutions.

HEX20

AX Electrical Power System (EPS)

The HEX20 AX Electrical Power System (EPS) is an EPS with 4 MPPT channels and a nominal bus voltage of 16.8V.

Bus Voltage (Nominal)	16.8 V
MPPT Channels	4
Input Voltage (Solar Panel)	>=18 V
Output Voltage	16.8 V
Maximum Output Current	3 A

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

50V Battery

Ibeos has completed the delivery of seven units of its new 50V, 1 kWhr battery, designed for missions requiring a radiation tolerant, highly mass-efficient, and reliable solution f

Voltage	50 V
Capacity	1 kWhr

price on request

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 @ 16 V

price on requestdatasheet

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
Supply voltage	22–33.6 V
Sustained discharge rate	10 A
Recommended charge rate	2.5 A
Heater power	20 W @ 28 V

price on requestdatasheet

ibeos

Ibeos Modular Power System (MPS)

The Ibeos Modular Power System (MPS) is a scalable power subsystem capable of delivering 500 to 2,000 Watts of power with high conversion efficiency.

Power Output	500 - 2,000 Watts
Power Conversion Efficiency	Up to 98%
TRL	9

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, 100 µm coverglass
BOL wing power	118 W at 25°C
Supply voltage	31-54V (typ. 42 V)
Bus current	2.6-3.0 A (typ. 2.8 A)

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.

Battery capacity	28.2 Wh
Battery capacity (2)	57.6 Wh
Supply voltage	3.3 V
Supply voltage (2)	5 V
Operating temperature	-40 to +80 °C

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 45 Wh per PBP, stackable for redundancy
Operating temperature	-40 to +70 °C
Storage temperature	-40 to +85 °C
Lifetime	12 months

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.

Mass	50 g
Mass (2)	100 g
Mass (3)	150 g
Mass (4)	300 g
Mass (5)	400 g

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.

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
Operating temperature	-40…+85 °C
Storage temperature	-50…+65 °C
Storage lifetime (at relative humidity < 60 %)	12 months
Battery Operational temperature (charge, heaters disabled)	+10…+45 °C

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

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

Supply 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

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 requestdatasheet

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	6.5 mm thick gimbal; 9 mm 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.

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

Body Mounted Solar Panels

SPM-SP is a modular and flexible family of solar panels by NPC Spacemind, designed for full compatibility with SM CubeSat structures and both commercial and custom-made CubeSat com

price on request

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-SP3X-L-1W

The D-SP3X-L-1W is a deployable solar panel designed for 3U/6U CubeSat structures, featuring a 1-wing lateral configuration and high-efficiency triple junction UTJ solar cells.

Peak power	8 - 8.8 W
Max power current	500 - 520 mA
Max power voltage	16 - 17.5 V
Open circuit voltage	18.2 - 19.3 V

price on requestdatasheet

NPC Spacemind

D-SP3X-L-2W

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

Configuration	2 Wings Lateral
Compatibility	3U/6U CubeSat structures
Solar Cells	High efficiency triple junction UTJ
Peak power	16 – 17.6 W
Power connectors	2 parallel picoblade

price on requestdatasheet

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

D-SP6X-L-2W

The D-SP6X-L-2W is a deployable solar panel system designed for 6U/12U CubeSat structures, featuring a 2-wing lateral configuration and high-efficiency triple junction UTJ solar ce

Compatibility	6U/12U CubeSat structures
Solar Cells	High efficiency triple junction UTJ
Peak Power	36.8 - 40 W
Power Connectors	4 parallel picoblade

price on requestdatasheet

NPC Spacemind

D-SP6X-V

The D-SP6X-V is a deployable solar panel designed for 6U/12U CubeSat structures, featuring high-efficiency triple junction UTJ solar cells and a vertical configuration.

Peak power	16.1 - 17.5 W
Max power current	1 - 1.04 A
Max power voltage	16.1 - 17.5 V
Open circuit voltage	18.2 - 19.3 V

price on request

NPC Spacemind

D-SP8X-L-1W

The D-SP8X-L-1W is a deployable solar panel designed for XY side integration, compatible with 8U/16U CubeSat structures and featuring high-efficiency triple junction UTJ solar cell

Configuration	1 Wing Lateral
Compatibility	8U/16U CubeSat structures
Solar Cells	High efficiency triple junction UTJ
Peak power	23 - 25 W
Max power current	1 – 1.04 A

price on requestdatasheet

NPC Spacemind

D-SP8X-L-2W

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

Peak power

46 - 50 W

price on requestdatasheet

NPC Spacemind

D-SP8X-V

The D-SP8X-V is a deployable solar panel system designed for 8U/16U CubeSat structures, featuring high-efficiency triple junction UTJ solar cells and a vertical configuration.

Peak power	23 - 25 W
Max power current	1 – 1.04 A
Max power voltage	23 - 25 V
Open circuit voltage	26 – 27.5 V

price on requestdatasheet

NPC Spacemind

Deployable Solar Panels

SM-D-SP is a family of Deployable Solar Panels designed by NPC SPACEMIND to provide a modular and flexible solution for nanosatellite applications.

price on request

NPC Spacemind

GEMINI – CUBESAT EPS

GEMINI is SPACEMIND’s Electrical Power System designed for CubeSats missions, featuring an integrated battery pack module with customizable input and output channels.

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 20 V
Battery packs	Up to 8 parallel battery packs
Battery pack capacity	84 Wh for 8 cells (per unit)
Output bus	Programmable Output Bus 3.3 V-5V-6/12 V-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

SP2Z

The SP2Z is a body-mounted solar panel designed for 6U/8U CubeSat structures, featuring high-efficiency triple junction UTJ solar cells.

Mass	80 g
Peak Power	4.6-5.2 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

SP4X

The SP4X is a body-mounted solar panel designed for 4U/8U CubeSat structures, featuring high-efficiency triple junction UTJ solar cells.

Mass	160 g
Peak Power	10.35-11.7 W
Current Max Power	500-520 mA
Voltage Max Power	20.7-22.5 V
Open Circuit Voltage	23.4-24.75 V

price on request

NPC Spacemind

SP4Z

The SP4Z is a body-mounted solar panel designed for the Z side of 12U/16U CubeSat structures, featuring high-efficiency triple junction UTJ solar cells.

Mass	180 g
Peak Power	9.2-10 W
Current Max Power	500-520 mA
Voltage Max Power	18.4-20 V
Open Circuit Voltage	20.8-22 V

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	~6970 cm^3
Bounding dimensions	43.9 cm x 13.6 cm x 11.6 cm
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 / 0.8 mm
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 / 0.8 mm
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.

Custom Solar Panels

Pumpkin, Inc. offers custom solar panels, including body-mounted and deployable options, designed for various space applications.

price on request

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 000datasheet

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 (8.4 V), 3S2P (12.6 V), 4S2P (16.8 V)
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, 5.2-8.4 V
Battery configuration option 3s2p	6 cells, 7.8-12.6 V
Battery configuration option 4s2p	8 cells, 10.4-16.8 V
Cell capacity option 1	2500 mAh (72 Wh with 8 cells)
Cell capacity option 2	3000 mAh (86 Wh 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 100 Wh 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.

MISC™ Solar Panel Arrays

Pumpkin, Inc. offers MISC™ Solar Panel Arrays, designed for various space applications.

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"/1.6 mm
Thickness option 2	0.031"/0.8 mm
Compatibility	Pumpkin CubeSat Kit solid-wall or skeletonized structures (Base Plate Assembly / Cover Pla
Maximum mass per panel (safety factor = 2)	500 g

$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

Pumpkin, Inc.

SUPERNOVA™ Standard Solar Panels

Pumpkin, Inc. offers SUPERNOVA™ Standard Solar Panels for space applications.

price on request

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	8.6 m
Mass	36 kg
BOL power	3.3 kW
Stowed width	2.32 m

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 requestdatasheet

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 requestdatasheet

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

MP 144350 xlr Li-ion Cell

3.65 V, 2.6 Ah (9.4 Wh) compact high-energy medium prismatic Li-ion cell with more than 1100 cycles at 100% DoD.

Chemistry	Li-ion
Typical capacity	2.6 Ah
Nominal voltage	3.65 V
Nominal energy	9.4 Wh
Max continuous discharge current	5.0 A

price on requestdatasheet

Saft

MP 174565 xtd CliP System 1s1p Battery

Single-cell 3.65 V, 4.0 Ah battery on the MP 174565 xtd cell with its own enclosure and protection circuit, -40 °C to +85 °C.

Chemistry	Li-ion
Configuration	1s1p
Typical capacity	4.0 Ah
Nominal voltage	3.65 V
Nominal energy	14.6 Wh

price on requestdatasheet

Saft

MP 174565 xtd Li-ion Cell

3.65 V, 4.0 Ah (14.6 Wh) medium prismatic Li-ion cell with an operating range of -40 °C to +85 °C.

Chemistry	Li-ion
Typical capacity	4.0 Ah
Nominal voltage	3.65 V
Nominal energy	14.6 Wh
Max continuous discharge current	8 A

price on requestdatasheet

Saft

MP 174865 xlr Li-ion Cell

3.65 V, 5.3 Ah (19.3 Wh) high-energy medium prismatic Li-ion cell with more than 950 cycles at 100% DoD.

Chemistry	Li-ion
Typical capacity	5.3 Ah
Nominal voltage	3.65 V
Nominal energy	19.3 Wh
Max continuous discharge current	10 A

price on requestdatasheet

Saft

MP 176065 xlr Li-ion Cell

3.65 V, 6.8 Ah (24.8 Wh) high-energy medium prismatic Li-ion cell with more than 1800 cycles at 100% DoD.

Chemistry	Li-ion
Typical capacity	6.8 Ah
Nominal voltage	3.65 V
Nominal energy	24.8 Wh
Max continuous discharge current	14 A

price on requestdatasheet

Saft

MP 176065 xtd Li-ion Cell

3.65 V, 5.6 Ah (20.4 Wh) medium prismatic Li-ion cell for -40 °C to +85 °C; the ExoMars Rover battery is built from MP 176065 xtd cells.

Chemistry	Li-ion
Typical capacity	5.6 Ah
Nominal voltage	3.65 V
Nominal energy	20.4 Wh
Max continuous discharge current	11 A

price on requestdatasheet

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	72 Ah (16 × 4.5 Ah VES16 cells; some listings quote 288 Ah)
Nominal energy	≈2,816 Wh (176 × 16 Wh cells; some listings quote 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

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

Saturn (Krasnodar) (ПАО «Сатурн») — Russian space industry enterprise, Krasnodar. Its products listed on NewSpace Market come from the Glavkosmos export catalogue.

Saturn (Krasnodar)

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
Design life	5 years
Lead time	4 months
Possibility to adapt the product to customer requirements	No
Capacity	90 Ah

price on request

Saturn (Krasnodar)

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
Design life	2 years
Lead time	4 months
Possibility to adapt the product to customer requirements	No

price on request