Development Status of the iodine Fed Advanced Cusp Field Thruster for Mid Power - iFACT-MP
Authors/Creators
Contributors
Project manager:
Project members:
Researchers:
- Kottke, Gerrit1
- Becke, Philipp1
- Ly, Jennifer1
- Sütterlin, Saskia1
- Vaupel, Max1
- Lopez, Pablo2
- Male, Fabien2
- Dandaleix, Louis2
- Faure, Ludovic2
- Dupenne, David3
- Deurveilher, Antoine4
- Sailler, Christophe4
- Wätzig, Katja5
- Schilm, Jochen5
- Fantoni, Gabriele6
- Scortecci, Fabrizio7
- Saravia, Manuel Martín8
- Bernazzani, Luca9
- Ceccarini, Alessio9
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1.
Airbus Defence and Space GmbH (Germany)
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2.
Airbus (France)
- 3. Sailler Airbus, Boulevard Jean Moulin, 78990 Élancourt, France
- 4. Airbus, Boulevard Jean Moulin, 78990 Élancourt, France
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5.
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
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9.
University of Pisa
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10.
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.
Files
IEPC2025-295_iFACT-MP_Kottke_v2.pdf
Files
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