CPM for GEO Feeder (TOP-M 260 mm)

  • Supporting & pointing an instrument (> 25 kg)
  • Parallel architecture
  • 3 identical linear actuators w/DC brushless & roller screws

Main objective

  • High performance & low RC
  • Targeting high quantities (e.g. constellation market)
  • No expensive high-perf optical encoders, roller-screws instead
  • Reduced electronics complexity (open loop control)


  • Demonstrator for Space Weather TBC


  •  Design to MAIT: TBD
  •  Assembly: TBD
  •  Test: TBD


RF equipment for satcom payload tests in thermal vaccum≈300 kg (2.5 m x 1 m x 1 m)

  • Assembly of 300 Ku/Ka waveguides, load, coax, etc…
  • Integration in  ISO 7 clean room.


Battery radiator assembly line

  • Airbus D&S Li-Ion battery radiator

Main objective

  • High thermal control performance & low RC for One Web constellation
  • High production rate: 3 radiator per day


  • Airbus One Web Satellites


  • Whole radiator supply chain management (active thermal control, thermal coating)
  • Industrialisation: fully optimised working station definition, quality control plan definition
  • ISO7 assembly at Comat’s facilities: 22 QM and 900+ FM