Published July 3, 2026 | Version v1

OVERVIEW OF THE IFACT-MP PROJECT: A EUROPEAN IODINE FED ADVANCED CUSP FIELD THRUSTER FOR MID-POWER

Authors/Creators

  • 1. ROR icon Airbus Defence and Space GmbH (Germany)
  • 1. ROR icon Airbus Defence and Space GmbH (Germany)
  • 2. Airbus, Bremen, Germany
  • 3. ROR icon Airbus (France)
  • 4. Airbus, Élancourt, France
  • 5. Fraunhofer IKTS, Dresden, Germany
  • 6. Aerospazio Tecnologie S.r.l., Rapolano Terme, Italy
  • 7. Universita Di Pisa, Pisa, Italy
  • 8. ROR icon EASN Technology Innovation Services BVBA
  • 9. ROR icon European Health and Digital Executive Agency
  • 10. University of Stuttgart, Stuttgart, Germany

Description

The iFACT-MP project aims to develop a 3–5 kW hybrid propulsion subsystem featuring an electric thruster configuration that utilizes an iodine-fed anode alongside a krypton-fed cathode. In parallel, a secondary development path focused on iodine-fed cathodes utilizing enhanced C12A7 emitters. Furthermore, other critical technologies for the subsystem were developed, such as the iodine fluidic chain, consisting of tank, flow regulator and heated pipework, as well as a breadboard PPU to manage the control loops and automated procedures. For system characterization, an in-situ optical mass flow meter was developed and an iodine-compatible vacuum facility equipped for high-power thrust and plume diagnostics was built. Following major milestones being achieved through component validation and coupling testing, the 
project is moving into a final endurance test campaign to verify system reliability and performance.  

Files

DocFinal-118-2284-(1).pdf

Files (972.8 kB)

Name Size Download all
md5:ec9460b09e4458d6dbda59010965901c
972.8 kB Preview Download