Power Systems — Space Hardware Marketplace

CubeSat Kit Fixed Solar Panel: End Panel

• SKU710-00764
• Panel Thickness0.031in / 0.8mm
• Solar Cell TypeTriple-junction solar cells, ~28% to >32% AM0 efficiency over product lifetime

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…

ST Engineering Power Control & Distribution Unit (PCDU)

Modular, scalable satellite power control and distribution unit delivering up to 4 kW with >97% conversion efficiency for…

SpaceTech Deployable Solar Arrays

• Fill ratio85%
• Panel size range< 0.5 m² (XS) to > 6 m² (XL) per panel
• Deployment technologyControlled, unsynchronized multi-hinge deployment using standardized C-spring hinges

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

SpaceTech SADA 44/22 (Solar Array Drive Assembly)

• Driving methodCurrent controlled, micro stepping
• Command interfaceUART (57.6kBaud); RS-422 or RS-485 available
• Supply voltage22V … 36V

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

GaAs end edge solar panel with coils

A GaAs solar panel with a built-in electromagnetic coil designed for CubeSat top/bottom edges, with a central aperture…

GaAs side solar panel with coils

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

Power supply system (with battery unit)

A two-module CubeSat EPS (SXC-PSS-03) consisting of a power system controller (SXC-PSU-03) and battery module (SXC-BAT-03) for solar…

High-power distribution and control unit

• Dimensions, mm244 x 171 x 45 (without fasteners)
• Mass, kg1.1
• Power voltage, V22-34

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

Regulation and control equipment

• Dimensions, mm306 x 161 x 140 (without fasteners)
• Mass, kg7
• Power voltage, V22-34

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

PPU-200 Power Processing Unit

• Anode powerUp to 230 W
• Input voltage26-36 V
• Operating temperature-35 to +80 C

Flight-proven power processing unit for LEO satellite Hall-effect thrusters.

PPU-1500 Power Processing Unit

Power processing unit for 1.5 kW-class electric propulsion systems.

PPU-500 Power Processing Unit

Power processing unit for 500 W-class Hall-effect thruster propulsion systems.

NANOeps-AMPPT

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

NANOeps

• StandardISO 19683, IPC Class 3+
• TRL9
• MAITIn-house

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

Amun

• Operating temperature-40 C to +85 C
• Dimensions95.9 x 90.2 x 19.7 mm (0.2U)
• Mass185 g

PC/104 form-factor power management unit for 0.5U-2U CubeSats.

Ra

• Operating temperature-40 C to +125 C
• Efficiency> 30%
• Configurations1U / 2U / 3U / 6U / 8U plus custom design

High-efficiency, customizable solar panels for nanosatellites, offered in 1U-8U and custom configurations.

Nanosatellite Power Subsystem

High-current, long-life lithium-ion nanosatellite battery and power management subsystem with flight heritage on 24+ satellites.

ABSL Li-ion Space Battery

• ChemistryLithium-ion (Li-ion)
• Voltage range12V to 151.2V (model dependent)
• Capacity range2Ah to 80Ah per standard model, larger multi-module up to 448Ah

EnerSys ABSL's flagship line of lithium-ion batteries purpose-built for spacecraft, offering configurable capacity, voltage, and power outputs for…