Space Hardware Marketplace

Magnetorquer

• Magnetic dipole moment to mass ratioHigh
• Power consumptionUnder 1W per A·sqm
• DesignCompact and lightweight

High-performance magnetic torquer for precise attitude control of CubeSats and SmallSats.

ADCS Unit

• Control axesTriaxial
• IntegrationMagnetorquers + reaction wheels + controller in single 3D-printed chassis
• Control approachAI-powered dynamic in-space control

Advanced AI-powered Attitude Determination and Control System combining magnetorquers, reaction wheels and controller in one 3D-printed chassis.

Electrical Power System (EPS)

• Capacity120 Wh (LFP-based)
• ArchitectureFully modular
• Power buses3.3V, 5V, 12V, & custom

Modular, high-density LFP-based power management system for SmallSats with 3.3V, 5V, 12V and custom power buses.

16U Satellite Platform

• Form factor16U
• Battery capacityOver 120 Wh
• Pointing systemAI-based triaxial pointing

Flagship 16U satellite platform with high-capacity battery, AI-based triaxial pointing, and bifacial solar cells.

NOEL-V RISC-V Processor IP Core

• ArchitectureRISC-V
• Issue widthUp to dual-issue (2 instructions/cycle)
• DeliverySynthesizable VHDL IP core (GRLIB)

Configurable synthesizable RISC-V processor IP core for space, offering dual-issue execution and flight-proven design.

LEON5 SPARC V8 Processor IP Core

• ArchitectureSPARC V8, 32-bit
• DeliverySynthesizable VHDL IP core (GRLIB)
• Target technologiesHigh-end FPGA, deep-submicron ASIC

Configurable synthesizable VHDL SPARC V8 processor IP core for FPGA and deep-submicron ASIC SoC designs.

GR718B Rad-Hard 18-Port SpaceWire Router

• Ports18 external SpaceWire ports + internal configuration/test ports
• Protocol complianceECSS-E-ST-50-12C, RMAP (ECSS-E-ST-50-52C), ECSS-E-ST-50-51C
• PackageCQFP-256, ceramic

Rad-hard 18-port SpaceWire router with RMAP configuration, flight-proven on ESA JUICE and other missions.

GR716A Rad-Hard LEON3FT Microcontroller

• Processor coreLEON3FT SPARC V8, fault-tolerant
• AnalogOn-chip ADC, DAC, POR, oscillator, brown-out detection, LVDS transceivers
• SupplySingle 3.3V

Rad-hard mixed-signal microcontroller with a fault-tolerant LEON3FT SPARC V8 processor for space and high-rel applications.

GR765 Octa-Core RISC-V/SPARC Rad-Hard SoC

• CoresUp to 8, RISC-V/SPARC
• Memory interfacesDDR2/DDR3/DDR4
• High-speed I/OSpaceFibre, WizardLink

Next-generation rad-hard system-on-chip with 8 RISC-V/SPARC cores, embedded FPGA, and integrated hardware security module.

GR740 Quad-Core LEON4FT SPARC V8 Processor

• Processor cores4x LEON4FT SPARC V8, fault-tolerant
• SpaceWire router8 ports
• Bus interfacesPCI initiator/target

Radiation-hardened quad-core LEON4FT SPARC V8 system-on-chip, ESA's Next Generation Microprocessor (NGMP).

MIME Thruster (Multimode Integrated Monopropellant Electrospray Thruster)

Dual-mode chemical/electrospray thruster for small satellites

ACS Test Bed

Air-bearing attitude control system test bench for small and micro satellites.

ASTROFEIN Gyro System AGS-1

Tri-axial gyro system with temperature-compensated data for small satellites.

ARGO-L1 GNSS Receiver Unit

Dual-redundant GPS L1 receiver unit for LEO satellite navigation.

ACM Magnetometer

High-precision magnetometer for attitude control, developed with Magson GmbH.

MicroCMG Control Moment Gyroscope

Compact control moment gyroscope delivering 14 Nm torque for small satellites.

PSL1U / PSL2U / PSL3U Picosatellite Launcher

Flight-proven CubeSat deployer family for 1U, 2U, and 3U CubeSats.

PSL6U / PSL6U XL Picosatellite Launcher

CubeSat deployer for 1U to 6U CubeSats with low-power, resettable mechanism.