Satellite Batteries

103 Satellite Batteries for Space Applications from 18 manufacturers listed on SatNow

Satellite Batteries are space-qualified energy storage systems designed to provide reliable electrical power to spacecraft subsystems during eclipse periods, peak load events, and transient operational modes. These batteries store energy generated by solar arrays and deliver regulated power to payloads, avionics, propulsion systems, and communication modules. Satellite Batteries for space applications from multiple manufacturers are listed on SATNow. Use the filters to select products based on your requirement. View product details, download datasheets, compare products, get quotes and pricing for matching products. SATNow has compiled this list of products specifically for Space and Satellite Applications.

103 Satellite Batteries from 18 Manufacturers
103 Products from 18 Manufacturers
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Description:High Energy Density Battery Array

Product Specs

Satellite Type:
CubeSat
Cell Chemistry:
Lithium Polymer
Mass:
209.45 g, 256.4 g, 227.7 g, 291.5 g, 216.7 g, 270.5 g
Capacity:
26 Wh, 52 Wh, 33.6 Wh, 67.2 Wh, 42 Wh, 84 Wh
Charge Current:
6.2 A, 8 A, 10 A, 12.4 A, 16 A, 20 A
Nominal Voltage:
3.7 V
Voltage Range:
3.7 to 8.4 V
more info
Description:3.4 Ah Flight Proven Spacecraft Battery

Product Specs

Mass:
675 gms
Capacity:
95.2 Wh
Nominal Voltage:
28 V
Voltage Range:
24 to 33.6 V
more info
Description:297 Wh Space-Qualified Lithium-ion Battery

Product Specs

Cell Chemistry:
Lithium Iron Phosphate
Mass:
4.80 gms
Capacity:
297 Wh
Discharge Current:
20 to 40 A
Nominal Voltage:
29.7 V
more info
Description:8.4 Ah Space-Qualified Li-Ion Rechargeable Battery

Product Specs

Satellite Type:
Smallsat
Cell Chemistry:
Lithium-Ion
Mass:
1660 gms
Capacity:
8.4 Ah, (248.64 Wh)
Nominal Voltage:
28
Voltage Range:
24 to 33.6 V
Storage Temperature:
0 to 45 Degree C (Discharge)
more info
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Description:52-62.5 Ah Lithium-Ion Secondary Cell

Product Specs

Cell Chemistry:
Lithium-Ion
Mass:
2020 gms
Capacity:
52 to 62.5 Ah / 204 to 245 Wh
Charge Current:
31.25 A
Discharge Current:
62.5 A (Constant), 125 A (Pulse)
Energy Density:
305.4 Wh/L
Storage Temperature:
-5 to 5 Degree C
more info
Description:23.1 V Lithium-Ferrite Modular Battery System for Small Satellites

Product Specs

Satellite Type:
SmallSat
Cell Chemistry:
Lithium-Ferrite, Lithium-Ion, Lithium Polymer
Mass:
3000 gms
Capacity:
172 Wh
Charge Current:
1 A
Nominal Voltage:
23.1 V
Power Consumption:
170 W
Voltage Range:
12 V, 15 V, 18 V, 28 V
Storage Temperature:
-20 to 40 Degree C
more info
Description:40 Wh CubeSat Battery for LEO Missions

Product Specs

Satellite Type:
Cubesat
Cell Chemistry:
Lithium Polymer
Mass:
335 gms
Capacity:
40 Wh
Charge Current:
2.6 A
Discharge Current:
2.6 A
Nominal Voltage:
6.2 V
Power Consumption:
0.10 W
Voltage Range:
3 to 8.4 V
Storage Temperature:
-20 to 60 Degree C
more info
Description:5-30 Ah Li-ion Battery For Microsatellites

Product Specs

Satellite Type:
MicroSat
Capacity:
5 to 25 Ah, (17.5 to 87.5 Wh)
Nominal Voltage:
2.75 to 4.2 V (3.5 V Single Battery)
Voltage Range:
12 to 42 V
more info
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Description:12Ah/45Wh Lithium-ion Cell for Space

Product Specs

Cell Chemistry:
Lithium-Ion
Mass:
390 gms
Capacity:
12 Ah / 45 Wh
Charge Current:
6 A
Discharge Current:
12 A
Nominal Voltage:
3.75 V
more info
Description:Lithium-Ion Battery

Product Specs

Cell Chemistry:
Lithium-Ion
Mass:
317 gms
Capacity:
2 x 3 Ah, (21.6 Wh)
Charge Current:
4 A
Discharge Current:
20 A
Nominal Voltage:
3.6 V
Voltage Range:
2.5 to 4.2 V
Storage Temperature:
-20 to 60 Degree C (Discharge)
more info
Description:Battery Module for CubeSats and Small Satellites

Product Specs

Satellite Type:
SmallSat, Cubesat, NanoSat
Cell Chemistry:
Lithium-Ion
Mass:
542 to 710 gms
Capacity:
72 to 100 Wh
Charge Current:
10 to 20 A
Discharge Current:
20 A
Nominal Voltage:
3.6 V
Power Consumption:
1 W
Voltage Range:
8.4 to 16.8 V
Storage Temperature:
-20 to 60 Degree C
more info
Description:14V Modular SmallSat Battery Missions

Product Specs

Satellite Type:
SmallSat
Cell Chemistry:
Lithium-Ion
Mass:
375 gms
Capacity:
45 to 90 Wh
Charge Current:
1.6 A
Discharge Current:
6.5 A
Nominal Voltage:
14 V
Power Consumption:
8 W
Voltage Range:
13.2 to 16.8 V
more info
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Description:4.5 Ah Spacecraft Battery for LEO Applications

Product Specs

Satellite Type:
MicroSat, NanoSat
Mass:
700 gms
Capacity:
4.5 Ah, (66.6 Wh)
Nominal Voltage:
14.8 V
Voltage Range:
13.2 to 16.4 V
Storage Temperature:
-20 to 10 Degree C
more info
Description:Strong, light weight structure Battery Pack with New 3D printing technology for aluminum

Product Specs

Mass:
1700 gms
Capacity:
154 Wh
Voltage Range:
4s4p : 12 to 16.4 V, 8s2p : 24 to 32.8 V
more info
Description:1700 Wh Satellite Battery for LEO Constellations

Product Specs

Cell Chemistry:
Lithium-Ion
Mass:
9.8 Kg
Capacity:
1147.5 to 1927.8 Wh
Charge Current:
15 A
Discharge Current:
15 A
Energy Density:
170 Wh/kg
Voltage Range:
22.5 to 37.8 V
more info
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What are Satellite Batteries?

Satellite Batteries are space-qualified energy storage systems designed to provide reliable electrical power to spacecraft subsystems during eclipse periods, peak load events, and transient operational modes. These batteries store energy generated by solar arrays and deliver regulated power to payloads, avionics, propulsion systems, and communication modules. The architecture typically consists of multiple electrochemical cells configured in series and parallel combinations, integrated with battery management electronics for charge control, cell balancing, protection, and health monitoring.

In orbital environments, battery systems must withstand radiation exposure, vacuum conditions, mechanical launch loads, and repetitive charge-discharge cycling across mission life. Performance characteristics such as voltage stability, current capability, and thermal behavior directly influence spacecraft power bus regulation and overall system reliability. Careful selection of chemistry, configuration, and electrical parameters ensures compliance with mission power budgets, safety requirements, and long-duration operational stability.

Key specifications of the Satellite Battery:

  • Satellite Type: Defines the class of host platform such as CubeSat, small satellite, or large spacecraft. Satellite type determines available volume, allowable mass, power demand profile, and mission duration, all of which directly affect battery sizing, redundancy strategy, and integration approach.
  • Cell Chemistry: Specifies the electrochemical system used within the battery, such as lithium-ion or other qualified chemistries. Cell chemistry influences energy density, cycle life, thermal characteristics, radiation tolerance, safety behavior, and charge management requirements.
  • Mass: Indicates the total mass of the battery assembly including cells, housing, interconnects, and management electronics. Mass affects launch cost, structural design, and spacecraft center-of-gravity considerations. Optimization of mass must be balanced against required energy storage and power capability.
  • Battery Capacity: Represents the total stored charge available for delivery, typically expressed in ampere-hours. Capacity determines the duration for which the spacecraft can operate without solar input and is a primary factor in eclipse survivability and mission endurance planning.
  • Charge Current: Defines the allowable current during the charging process. Charge current limits impact recharge time, thermal generation, and long-term cell degradation. Proper alignment with solar array output and power conditioning systems is essential to maintain battery health.
  • Discharge Current: Specifies the maximum continuous or peak current that can be delivered to spacecraft loads. Discharge capability determines support for high-power subsystems and transient operational modes, influencing voltage stability and thermal management requirements.
  • Voltage Range: Indicates the permissible operating voltage window across charge and discharge states. The voltage range must align with spacecraft power bus tolerances and ensures compatibility with downstream converters and protection circuitry.
  • Nominal Voltage: Represents the reference operating voltage of the battery under standard conditions. Nominal voltage determines series cell configuration and integration compatibility with regulated and unregulated power bus architectures.
  • Power Consumption: Refers to the electrical demand imposed by connected spacecraft subsystems that the battery must support during non-generation phases. Understanding power consumption profiles is essential for accurate capacity sizing, thermal analysis, and lifecycle performance assurance.

The Largest Database of Satellite Batteries

SatNow has listed Satellite Batteries from the leading manufacturers and made them searchable by specification. You can enter the key parameters and the search tool will scan catalogs from the leading manufacturers to identify products that meet your spec. Once you find Satellite Batteries that meet your requirement, you can view product information, download datasheets or request quotations. Quotation requests will be routed to the manufacturer of the product who will get back to you directly. The quotation will also be routed to distributors of the product in your region.