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.

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

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.)

VIDEO (2019)

Video Imaging Demonstrator for Earth Observation

Read More  

GALACTIC (2020)

High Performance Alexandrite Crystals and Coatings for High Power Space Applications

Read More  

AETHER (2019)

Air-breathing Electric THrustER

Read More