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EDDA SIGNED

European Direct-Drive Architecture

Total Cost €

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EC-Contrib. €

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Partnership

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 EDDA project word cloud

Explore the words cloud of the EDDA project. It provides you a very rough idea of what is the project "EDDA" about.

sitael    reduce    designed    voltage    mass    mission    space    power    transversal    roadmaps    saving    adaptable    plasma    vacuum    solar    cathod    advantages    het    optimizing    illumination    maximize    drive    demonstration    sun    spain    28    consumption    off    tests    innovation    400v    hempt    efficiency    quick    significantly    conversion    bus    tugs    easily    performed    hardware    demonstrator    thruster    satellites    multistage    100v    carriers    variation    thales    save    remove    tools    converters    technologies    switch    loop    edda    provides    efficient    architecture    germany    heart    corresponds    technological    effect    italy    orbit    complete    reference    servicing    thrust    point    telecommunication    300v    manufactured    chamber    electric    tas    spacecraft    thrusters    array    electronics    follow    satellite    propulsion    demonstrated    chain    hall    vs    interplanetary    innovative    uc3m    dissipation    direct    supplies    start    thermal    robustness    time   

Project "EDDA" data sheet

The following table provides information about the project.

Coordinator
THALES ALENIA SPACE FRANCE SAS 

Organization address
address: AVENUE JEAN FRANCOIS CHAMPOLLION 26
city: TOULOUSE
postcode: 31100
website: www.thalesaleniaspace.com

contact info
title: n.a.
name: n.a.
surname: n.a.
function: n.a.
email: n.a.
telephone: n.a.
fax: n.a.

 Coordinator Country France [FR]
 Total cost 998˙023 €
 EC max contribution 998˙023 € (100%)
 Programme 1. H2020-EU.2.1.6.1. (Enabling European competitiveness, non-dependence and innovation of the European space sector)
2. H2020-EU.2.1.6.2. (Enabling advances in space technology)
 Code Call H2020-SPACE-2019
 Funding Scheme RIA
 Starting year 2019
 Duration (year-month-day) from 2019-12-01   to  2021-11-30

 Partnership

Take a look of project's partnership.

# participants  country  role  EC contrib. [€] 
1    THALES ALENIA SPACE FRANCE SAS FR (TOULOUSE) coordinator 235˙483.00
2    SITAEL SPA IT (MOLA DI BARI) participant 249˙750.00
3    THALES ALENIA SPACE BELGIUM S.A. BE (MONT SUR MARCHIENNE) participant 202˙155.00
4    EFFICIENT INNOVATION SAS FR (CASTELNAU LE LEZ) participant 109˙250.00
5    THALES DEUTSCHLAND GMBH DE (DITZINGEN) participant 101˙307.00
6    UNIVERSIDAD CARLOS III DE MADRID ES (GETAFE (MADRID)) participant 100˙077.00

Map

 Project objective

The European Direct-Drive Architecture (EDDA) project aims at optimizing the power chain efficiency of a spacecraft using electric propulsion, which is at the heart of technological roadmaps for future spacecraft.

The objective is to develop, build and test a demonstrator of a high voltage and high power direct-drive concept.

This innovative architecture supplies directly electric thrusters by a 300V-400V Solar Array without power conversion vs 28-100V in the current state of the art. The advantages are to remove power converters, to save mass, dissipation and cost, and to improve significantly the overall efficiency and reduce the thermal dissipation. In addition, at satellite level, it corresponds to a reduction of thrust duration, saving mission time.

The ability of the concept to be applied to various thrusters technologies is key to maximize the impact of the architecture. Therefore this study is based on a transversal aspect of Electric Propulsion to be demonstrated on two different Electric Thruster technologies: Hall Effect Thruster (HET) from Sitael (Italy) and High Efficiency Multistage Plasma Thruster (HEMPT) from Thales-D (Germany).

EDDA demonstration is based on a thruster plasma analysis (UC3M, Spain). Cathod Reference Point electronics, HET, vacuum chamber for complete testing are provided by Sitael. The bus voltage control loop and associated hardware are designed and manufactured by TAS-B. Coordination at satellite level is performed by TAS-F. And Efficient Innovation provides effective management and associated tools.

Tests will follow real operational conditions: no Sun, variation of illumination, thruster start-up and switch off, quick variation of consumption, and will demonstrate the robustness of this architecture easily adaptable to spacecraft (telecommunication satellites for Electric Orbit Raising reduction, In Orbit Servicing and Space-tugs, interplanetary carriers).

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The information about "EDDA" are provided by the European Opendata Portal: CORDIS opendata.

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