Examples of our projects in the Space, Defense, Industrial and Civil sectors
A rack system reconciling the electrical interfaces between an in-service test bench and a newly designed orbital module. System design, mechanical and electronic development, support to integration and AIT.
SpaceHarness design and build, cabinet integration and support to AIT on an observation payload data chain.
SpaceEnclosed test benches for railway gearboxes and wheelsets, with operating and acquisition software and CE marking. Electrical design, control software, documentation, risk analysis for CE marking, and conduct of the test campaign.
TransportSystem and subsystem hardware design and integration for a launcher control bench, with support to AIT both in factory and on site.
SpaceThe cabinets from which a launch vehicle is powered, commanded and monitored before lift-off, and the installation that connects them to the vehicle. Full cycle through to installation at the launch base.
SpaceA rack system with a controller managing up to five charger modules, each able to charge two batteries. System design, mechanical and electronic development, support to integration and AIT.
SpaceA drawer bringing out the LVDS interfaces of an on-board mass-memory unit, with the matching harness built for clean-room use. Support to CE certification of the complete unit, not of the drawer alone.
SpaceA drawer with plug-in boards carrying the telecommand and telemetry interfaces to an observation payload's data chain, with a motherboard and purpose-built daughter boards, one per signal family.
SpaceA rack system that acquires telemetry and routes it over a satellite relay link. System hardware design, software development, power distribution unit, internal cabling, integration and configuration, support to AIT.
SpaceA 19" rack RF switch matrix with settable attenuation and local or remote operation. Component responsibility: design, hardware integration, software and AIT.
SpaceA second application of the RF matrix, for the test chain of an Earth-observation microwave radiometer. Delivered CE marked, with a web-server HMI.
SpaceA work-holding system replacing a set of dedicated jigs with a single reconfigurable fixture for blades of varying geometry. System design, mechanical, electronic and software development, on-site installation and AIT.
IndustrialA board that switches RS-422 differential serial links with the logic implemented as FPGA firmware, and a unit that detects a radio-frequency signal and commands path switching with microcontroller firmware. Electrical design, board build, firmware design and development.
SpaceFull design of an EGSE cabinet for the data chain of an Earth-observation satellite, including all 3D modelling and custom cables, and electrical and mechanical design of a power supply SCOE for a launch vehicle. A design office delivering a design, not a box.
SpaceAssembly integration of rack sub-assemblies housed in stackable shock-mounted cases, with instrumentation, per-line protected power distribution and external interconnection cabling.
SpaceA unit that decouples the check-out chain from the item under test and verifies its integrity before connection. Subcomponent mechanical and electronic design, and support to AIT.
SpaceA SCOE providing the links between the vehicle control bench and the embarked payloads. Full cycle: electrical and mechanical design, procurement, documentation, assembly drawings, AIT and installation at the launch base.
SpaceA SCOE for a satellite payload's communication chain. Support to system and subsystem hardware and software design, software development, AIT at factory acceptance (FAT) and on-site acceptance (OSAT).
SpaceA SCOE simulating the behaviour of a radar payload, across two instrumented cabinets. Support to hardware and software design, system and subsystem software development, AIT conducted at FAT and OSAT.
SpaceThe telemetry section of a launch vehicle control bench: it receives, decodes and presents vehicle parameters to the operators. System hardware design, integration and configuration, support to AIT.
SpaceBoth interface sections of one automatic test equipment — telemetry and telecommand, command and control of the radio-frequency chain — in integrated chassis, operated through an on-board web server. Subcomponent responsibility and support to AIT, as a subcontractor to a third-party integrator.
SpaceA cabinet that replaces a launch vehicle's real pyrotechnic circuits with electrically equivalent loads, and a simulator presenting the control bench with the loads of the on-board users. System responsibility, mechanical and electronic development, AIT.
SpaceA rack system that reduces the manual work required of the electrical operator to revalidate the control bench interfaces after a launch. System design, mechanical and electronic development, support to integration and AIT.
SpaceA 19" rack antenna control unit, with front-panel controls and an operator interface served by an on-board web server. Full system responsibility, from architecture through to on-site installation.
SpaceA family of rack power distribution units, with input and output voltage and current metering, per-group protection and emergency stop. Design, engineering, production and integration into different EGSE systems.
SpaceA transportable RF check-out system, designed and developed in hardware and software, including the power distribution unit and four purpose-built interface subsystems.
Defence