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E.T.PACK SIGNED

Electrodynamic Tether Technology for Passive Consumable-less Deorbit Kit

Total Cost €

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EC-Contrib. €

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Partnership

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 E.T.PACK project word cloud

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

opening    combining    ca24al28o64    operation    radiation    reversible    interdependent    electrodynamic    physics    c12a7    compensated    magnetic    edge    tether    proof    space    propulsion    coating    material    magnetosphere    thermal    flight    interacts    thermionic    cutting    demonstrator    designed    optical    conductive    uv    electride    photoelectric    constraints    equipped    enhances    risk    lwts    4e    extraordinary    electrical    deorbit    active    manufacture    theory    tethers    accurate    horizons    passively    scenarios    consumables    placed    framework    kit    readiness    plasma    mechanism    de    passive    first    solar    emissions    lwt    boost    orbit    cathode    survivability    ambient    tape    atox    modes    momentum    re    deployment    pack    impossible    solid    electron    mechanical    simulators    function    planet    exchange    interdisciplinary    charge    frontier       coated    spacecraft    explored    comparisons    science    free    backup    conventional    hitherto    resistance    mission    experiment    breaking    environment    hollow    simulator    mode   

Project "E.T.PACK" data sheet

The following table provides information about the project.

Coordinator
UNIVERSIDAD CARLOS III DE MADRID 

Organization address
address: CALLE MADRID 126
city: GETAFE (MADRID)
postcode: 28903
website: http://www.uc3m.es

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 Spain [ES]
 Total cost 3˙039˙977 €
 EC max contribution 2˙999˙999 € (99%)
 Programme 1. H2020-EU.1.2.1. (FET Open)
 Code Call H2020-FETOPEN-2018-2019-2020-01
 Funding Scheme RIA
 Starting year 2019
 Duration (year-month-day) from 2019-03-01   to  2022-05-31

 Partnership

Take a look of project's partnership.

# participants  country  role  EC contrib. [€] 
1    UNIVERSIDAD CARLOS III DE MADRID ES (GETAFE (MADRID)) coordinator 468˙587.00
2    TECHNISCHE UNIVERSITAET DRESDEN DE (DRESDEN) participant 699˙275.00
3    SENER INGENIERIA Y SISTEMAS SA ES (GETXO) participant 643˙659.00
4    FRAUNHOFER GESELLSCHAFT ZUR FOERDERUNG DER ANGEWANDTEN FORSCHUNG E.V. DE (MUNCHEN) participant 638˙975.00
5    UNIVERSITA DEGLI STUDI DI PADOVA IT (PADOVA) participant 401˙125.00
6    ADVANCED THERMAL DEVICES S.L. ES (ALCORCON) participant 148˙377.00

Map

 Project objective

The Low Work-function Tether (LWT) is a long conductive tape coated with a material that enhances thermionic and photoelectric electron emissions. It enables spacecraft to de-orbit and/or re-boost without the need for consumables. It interacts passively with its environment (ambient plasma, magnetic field and solar radiation) to exchange momentum with the planet’s magnetosphere. E.T.PACK aims at developing a proof of concept for LWTs by breaking through and combining the current frontier of knowledge in three fields: plasma physics, low work function material science and space tethers. These will be integrated into a deorbit kit and a flight simulator for mission analysis. The kit aims to reach Technology Readiness Level 4 and will have two modes of operation: as a fully passive LWT and as a conventional electrodynamic tether equipped with an active hollow-cathode (backup mode). A new coating process for the electride, C12A7 ([Ca24Al28O64]4(4e-)), will be developed, and used to manufacture a LWT demonstrator. The C12A7 and its extraordinary properties will be also applied to the hollow cathode of the kit, which will include a novel deployment mechanism specifically designed for LWT applications. The complex current exchange of LWTs with the ambient plasma under space-charge-conditions will be studied theoretically, and used to develop accurate simulators. The theory-experiment comparisons will lead to a solid framework for LWT operation and constraints, including thermal, mechanical, optical, electrical, ATOX and UV resistance, and survivability. Hitherto impossible mission scenarios will be explored, thus opening up new horizons in space science and technology. These interdisciplinary activities, placed at the cutting edge of their fields and highly interdependent, make E.T.PACK a high-risk project. This is fully compensated by its potential impact: Europe being the first with access to a reversible in-space propulsion technology free of consumables.

 Publications

year authors and title journal last update
List of publications.
2020 G. Sánchez-Arriaga, J.R. Sanmartín
Electrical model and optimal design scheme for low work-function tethers in thrust mode
published pages: 105519, ISSN: 1270-9638, DOI: 10.1016/j.ast.2019.105519
Aerospace Science and Technology 96 2020-04-21
2020 G. Sanchez-Arriaga, S. Naghdi
Ionospheric Experiment with a Low Work Function Tether Loop
published pages: 212-221, ISSN: 1533-3884, DOI: 10.2514/1.g004746
Journal of Guidance, Control, and Dynamics 43/2 2020-04-21
2019 Wätzig, Katja; Rost, Axel; Schilm, Jochen; Tajmar, M.; Michaelis, Alexander
Contacting Methods for C12A7 Electride Ceramic
published pages: , ISSN: 2190-9385, DOI: 10.4416/JCST2019-00032
Fraunhofer IKTS 1 2020-04-21

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The information about "E.T.PACK" are provided by the European Opendata Portal: CORDIS opendata.

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