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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.

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

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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