Openfund

CORDIS · iFACT

iFACT - Iodine Fed Advanced Cusp field Thruster

Code
iFACT
Programme
H2020
Call
SPACE-13-TEC-2019
Status
CLOSED
Period
2020-01-01 – 2022-06-30
Total cost (whole consortium)1 999 595 €
EU contribution (whole consortium)1 999 595 €
EU contribution to Bulgarian participants110 000 €

Official data · CORDIS · synced 2026-10-18 03:29 · official record

Participants

OrganisationsRoleCountryGrant
AIRBUS DEFENCE AND SPACE GMBHcoordinatorDE909 688 €
AEROSPAZIO TECNOLOGIE SRLparticipantIT400 000 €
UNIVERSITY OF SOUTHAMPTONparticipantUK198 445 €
EASN TECHNOLOGY INNOVATION SERVICES BVBAparticipantBE116 250 €
ЕНДУРОСАТ ЕАДparticipantBG110 000 €
FRAUNHOFER GESELLSCHAFT ZUR FORDERUNG DER ANGEWANDTEN FORSCHUNG EVparticipantDE100 424 €
JUSTUS-LIEBIG-UNIVERSITAET GIESSENparticipantDE99 958 €
AIRBUS DEFENCE AND SPACE SASparticipantFR64 831 €

Description

Since several years, the industrialisation of the satellite market has been accelerated. In particular, the market for telecom satellites has changed significantly, because of several new players and numerous plans for satellite constellations, such as OneWeb or Starlink.In order to increase competitiveness and to disrupt the electric propulsion market, we are proposing the development of the iodine Fed Advanced Cusp field Thruster (iFACT).iFACT consists of an Advanced Cusp Field Thruster (ACFT), a simple PPU, a thermionic Emitter, a novel propellant feeding architecture, which is optimised for iodine. The ACFT has been invented by Airbus in 2017. Due to its simplicity, paired with efficiency, the fact that it is easy to ignite and its excellent performance data with iodine, it is tailored as key element for an extremely simple, efficient and low cost Electric Propulsion Subsystem (EPS). The baseline thruster (300 W input power) can be used with a simple thermionic cathode. The simple operation of the ACFT enables a reduced (wrt. number of parts and control circuits) but efficient PPU. This components are paired with an unique iodine feeding architecture which is capable to disrupt the electric propulsion market.Based on this, the proposal will focus on:- Iodine as disruptive propellant for electric thruster,- maturation of the Advanced Cusp Field Thruster (ACFT) as disruptive thruster principle, in three different power classes,- development of an novel, disruptive, extremly simplified low cost Power Processing Unit (PPU),- use of calcium aluminate (C12A7) as disruptive, low-work function emitter material for cathodes,- development of an European Iodine compatible long firing test facility.

Official data · CORDIS · synced 2026-10-18 03:29 · official record · Licence: © European Union, CC BY 4.0 (Commission reuse policy).