Space Hardware Marketplace

Z7000-P4

• MSRP€18,000
• ProcessorDual-core ARM Cortex-A9 MP-Core with NEON SIMD
• FPGA logic125K programmable cells

Versatile payload and onboard computing platform based on a dual-core ARM Cortex-A9 SoC with integrated FPGA logic.

OBC

• MSRP€9,000
• ArchitectureFour independent ARM Cortex-M7 modules
• Operating systemFreeRTOS

Quad-core ARM Cortex-M7 onboard computing platform for redundant mission-critical satellite functions.

GNC Platform

• 6U CubeSat pointing accuracy< 2 deg (WHL-P4 + FSS + IMU-P4)
• 16U CubeSat pointing accuracy0.1-0.5 deg (STR + WHL-P4 + FSS + IMU-P4)
• Microsat 50-200 kg pointing accuracy50 arcsec (Dual STR + WHL-P4 + FSS + IMU-P4)

Complete, scalable Guidance, Navigation and Control system combining sensors, actuators and control software for CubeSats and MicroSats.

6U AIS/VDES

• MSRPFrom €870,000
• Antenna3-element crossed deployable yagi antenna
• Mission focusAIS/VDES maritime communication and navigation

6U maritime AIS/VDES satellite with a 3-element crossed deployable yagi antenna for maritime communication and navigation.

6U Tactical Communications

• MSRPFrom €1,200,000
• Mission life10 years
• SecurityAES-256 encryption; SSH, WebAPI and password access protections

High-performing 6U satellite for secure, tactical communication between space and Earth with a 10-year mission life.

16U Hyperspectral 200mm

• MSRPFrom €1,100,000
• Telescope aperture200 mm
• Payload typeHyperspectral imaging

16U CubeSat equipped with a 200mm hyperspectral telescope for scientific and environmental observation missions.

16U GEO for BIU

• MSRPFrom €3,000,000
• Orbit raising1200 km raise, journey of more than 28 million km to first GEO service slot
• BandsKa, Ku and other bands

16U Bring-Into-Use (BIU) CubeSat designed for direct injection into geostationary orbit using Ka, Ku and other bands.

Geostationary BIU Microsatellite

• MSRPFrom €4,500,000
• Launch orbitLEO or GTO
• Target orbitGeostationary Orbit

Small ESPA-class geostationary communications microsatellite engineered for LEO or GTO launch with onboard propulsion for orbit raising.

ESM Satellite Platform

• MSRPFrom €4,500,000
• Mission focusElectronic Support Measures (ESM) - radar signature detection and geolocation

Microsatellite platform configured for Electronic Support Measures (ESM) missions with hi-reliability, shielded subsystems.

6U Satellite

• Mission life10 years
• SecurityAES-256 encryption, multiple access protections
• Payload volumeUp to 4U

Dependable 6U CubeSat platform for secure and tactical communication with a 10-year mission life.

8U Satellite

• Reaction wheels100 mNms
• Star trackerStandard, dual optional for enhanced pointing accuracy
• RedundancyDual communication and battery buses

High-performance 8U CubeSat with reaction wheels, star tracker and dual redundant buses for demanding missions.

12U Satellite

• Reaction wheelsFour 100 mNms reaction wheels
• Star trackers (optional)Dual star trackers, 10-20 arcsec pointing accuracy
• Sun sensorsSix fine sun sensors

Modular 12U CubeSat with electric propulsion and reaction wheels for high manoeuvrability and precise attitude control.

16U Satellite

• Momentum capacity100 mNms
• Torque capability20 mNm
• Payload accommodationUp to 12U depending on orbit requirements

High-performing 16U CubeSat platform with GEO options and flight heritage in both GEO and LEO.

BIG CAT 600

ESPA Grande-class microsatellite platform (up to 600 kg) with full-plate payload adapter for heavy-duty missions.

BIG CAT 300

ESPA-class microsatellite platform (up to 300 kg) with half-plate payload adaptor for high-demand missions.

BIG CAT 100

ESPA-class microsatellite platform (up to 100 kg) built from flight-proven, in-house modules for a quarter-plate payload adapter.

Mining & Raw Materials Environmental Monitoring

3D DEM and satellite-imagery based environmental and landslide risk monitoring service for mining sites.

Crisis Management Web-GIS Platform

Modular web-GIS decision-support platform for crisis planning, simulation and response, based on the CRISMA project.