Published February 27, 2026 | Version v1
Conference proceeding Open

Development Status of the iodine Fed Advanced Cusp Field Thruster for Mid Power - iFACT-MP

  • 1. ROR icon Airbus Defence and Space GmbH (Germany)
  • 2. ROR icon Airbus (France)
  • 3. Sailler Airbus, Boulevard Jean Moulin, 78990 Élancourt, France
  • 4. Airbus, Boulevard Jean Moulin, 78990 Élancourt, France
  • 5. ROR icon Fraunhofer Institute for Ceramic Technologies and Systems
  • 6. Aerospazio Tecnologie S.r.l., Via Provinciale Nord 42a, 53040 Rapolano
  • 7. Aerospazio Tecnologie S.r.l., Via Provinciale Nord 42a, 53040 Rapolano Terme, Italy
  • 8. Universita Di Pisa, Lungarno Pacinotti 43, 56126 Pisa, Italy
  • 9. ROR icon University of Pisa
  • 10. ROR icon EASN Technology Innovation Services BVBA

Description

iFACT-MP targets to develop a hybrid propulsion subsystem with a thruster unit consisting of an iodine fed anode and a krypton fed cathode as baseline in the 3-5 kW range. In parallel of the thruster unit, an iodine fed cathode is under development using enhanced C12A7 emitters. Further work is performed on the essential iodine specific building blocks such as the iodine fluidic chain, consisting of tank, regulator and heated pipework, as well as a Breadboard PPU to drive all functions, control loops and procedures. An optical mass flow meter allows in-situ measurement of the flow rate, and an iodine compatible vacuum test facility with thrust and plume diagnostics is built for this power range. At the current stage, all building blocks are integrated and have been individually tested, with coupling tests at increasing levels of integration to come. 

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IEPC2025-295_iFACT-MP_Kottke_v2.pdf

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