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iFACT - Iodine Fed Advanced Cusp field Thruster

Descrizione del progetto

Propulsori alimentati a iodio per la propulsione satellitare

In un contesto di mercato satellitare dinamico, il propulsore a campo cuspidale avanzato alimentato a iodio (iFACT) punta a rivoluzionare lo stato attuale della tecnologia di propulsione elettrica. Il propulsore a campo cuspidale avanzato (advanced cusp field thrusted, ACFT) è stato sviluppato da Airbus nel 2017. Le sue caratteristiche presentano un notevole potenziale di semplicità, efficacia e bassi costi nei sottosistemi di propulsione elettrica. Il propulsore è facile da accendere ed è ottimizzato per andare a iodio, avendo dimostrato eccellenti risultati prestazionali. La prospettiva per lo iodio quale propellente innovativo e per ACFT quale propulsore principale per sostituire la consolidata tecnologia sarà ulteriormente esplorata tra le altre aree di interesse, nel quadro de progetto iFACT, finanziato dall’UE.

Obiettivo

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.

Invito a presentare proposte

H2020-SPACE-2018-2020

Vedi altri progetti per questo bando

Bando secondario

H2020-SPACE-2019

Meccanismo di finanziamento

RIA - Research and Innovation action

Coordinatore

AIRBUS DEFENCE AND SPACE GMBH
Contribution nette de l'UE
€ 909 687,50
Indirizzo
WILLY-MESSERSCHMITT-STRASSE 1
82024 Taufkirchen
Germania

Mostra sulla mappa

Regione
Bayern Oberbayern München, Landkreis
Tipo di attività
Private for-profit entities (excluding Higher or Secondary Education Establishments)
Collegamenti
Costo totale
€ 909 687,50

Partecipanti (7)