Opendata, web and dolomites

EDDA SIGNED

European Direct-Drive Architecture

Total Cost €

0

EC-Contrib. €

0

Partnership

0

Views

0

 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.

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

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).

Are you the coordinator (or a participant) of this project? Plaese send me more information about the "EDDA" project.

For instance: the website url (it has not provided by EU-opendata yet), the logo, a more detailed description of the project (in plain text as a rtf file or a word file), some pictures (as picture files, not embedded into any word file), twitter account, linkedin page, etc.

Send me an  email (fabio@fabiodisconzi.com) and I put them in your project's page as son as possible.

Thanks. And then put a link of this page into your project's website.

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

More projects from the same programme (H2020-EU.2.1.6.1.;H2020-EU.2.1.6.2.)

GALACTIC (2020)

High Performance Alexandrite Crystals and Coatings for High Power Space Applications

Read More  

NEMESIS (2019)

Novel Electride Material for Enhanced electrical propulSIon Solutions

Read More  

IMPACTA (2019)

Innovative Mechanically Pumped loop for ACtive Antennae

Read More