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CHEOPS SIGNED

Consortium for Hall Effect Orbital Propulsion System

Total Cost €

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EC-Contrib. €

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Partnership

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Project "CHEOPS" data sheet

The following table provides information about the project.

Coordinator
SAFRAN AIRCRAFT ENGINES 

Organization address
address: BVD DU GENERAL MARTIAL VALIN 2
city: PARIS
postcode: 75015
website: www.safran-aircraft-engines.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]
 Project website https://www.cheops-h2020.eu/
 Total cost 14˙792˙359 €
 EC max contribution 10˙960˙028 € (74%)
 Programme 1. H2020-EU.2.1.6.2. (Enabling advances in space technology)
2. H2020-EU.2.1.6.1.1. (Safeguard and further develop a competitive, sustainable and entrepreneurial space industry and research community and strengthen European non-dependence in space systems)
 Code Call H2020-COMPET-2016
 Funding Scheme IA
 Starting year 2016
 Duration (year-month-day) from 2016-11-01   to  2020-04-30

 Partnership

Take a look of project's partnership.

# participants  country  role  EC contrib. [€] 
1    SAFRAN AIRCRAFT ENGINES FR (PARIS) coordinator 4˙283˙049.00
2    SITAEL SPA IT (MOLA DI BARI) participant 2˙089˙806.00
3    BRADFORD ENGINEERING BV NL (HEERLE) participant 1˙052˙205.00
4    CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE CNRS FR (PARIS) participant 1˙014˙339.00
5    AST ADVANCED SPACE TECHNOLOGIES GMBH DE (OSTERHOLZ-SCHARMBECK) participant 651˙931.00
6    THALES ALENIA SPACE BELGIUM S.A. BE (MONT SUR MARCHIENNE) participant 600˙071.00
7    UNIVERSIDAD CARLOS III DE MADRID ES (GETAFE (MADRID)) participant 360˙001.00
8    CHALMERS TEKNISKA HOEGSKOLA AB SE (GOETEBORG) participant 332˙012.00
9    DEUTSCHES ZENTRUM FUER LUFT - UND RAUMFAHRT EV DE (KOELN) participant 175˙696.00
10    SME4SPACE VZW BE (HEVERLEE) participant 135˙874.00
11    OHB SYSTEM AG DE (BREMEN) participant 94˙705.00
12    AIRBUS DEFENCE AND SPACE SAS FR (TOULOUSE CEDEX) participant 92˙750.00
13    THALES ALENIA SPACE FRANCE SAS FR (TOULOUSE) participant 77˙585.00

Map

 Project objective

CHEOPS proposes to develop three different Hall Effect Thruster electric propulsion systems: a dual mode EPS for GEO applications, a low power for LEO applications and a >20 kW high thrust EPS for exploration applications. Each of these will be developed according to market needs and drivers applying incremental technology changes to existing EPS products. The development approach will follow the ESA ECSS approach and the dual mode and low power are targeting a System PDR review with 42 months from the project start. Development will cover the following elements: thruster, cathode, PPU and FMS. The project is perfectly aligned to the SRC guidelines published with the call. Through a detailed development plan the project will demonstrate their ability to achieve by the end of CHEOPS Phase II (2023) the following: a) TRL7-8 for dual mode and low power b) high power HET EPS TRL6. Common transverse activities will include advanced numerical design tools for electric propulsion which will further the understanding of the observable behaviour and interactions with the satellite platform and predict performances of a given design. This includes alternative propellants and the ability to estimate the system lifetime. Finally significant progress will be made in establishing a HET performances measurement standard and developing advanced non-intrusive tests for measuring thruster erosion. The CHEOPS consortium is led by SNECMA and is comprised of representatives of the biggest European Prime satellite makers, the full EPS supply chain and supported by academia.

 Deliverables

List of deliverables.
CHEOPS public website Websites, patent fillings, videos etc. 2020-04-08 11:01:30

Take a look to the deliverables list in detail:  detailed list of CHEOPS deliverables.

 Publications

year authors and title journal last update
List of publications.
2018 Eric Bourguignon, Stéphane Fraselle
Power Processing Unit Activites at Thales Alenia Space in Belgium
published pages: , ISSN: , DOI:
Space Propulsion Proceedings 2018 2020-04-08
2017 Eric Bourguignon, Stéphane Fraselle
PPU Mk3 for 5 kW Hall Effect Thrusters
published pages: , ISSN: , DOI:
IEPC Conference Proceeding 2017-171 2020-04-08
2018 Tommaso Andreussi, Antonio Piragino, Eugenio Ferrato, Maryam Reza, Farbod Faraji, Giulia Becatti, Daniela Pedrini, Alena Kitaeva, Angela Rossodivita, Mariano Andrenucci
HT20k Hall Thruster development status
published pages: , ISSN: , DOI:
69th International Astronautical Congress (IAC), Bremen, Germany, 1-5 October 2018. IAC-18 2020-04-08
2018 Ms. Martina Mammarella, Politecnico di Torino, Italy; Mr. Christopher Andrea Paissoni, Politecnico di Torino, Italy; Dr. Roberta Fusaro, Politecnico di Torino, Italy; Prof. Nicole Viola, Politecnico di Torino, Italy; Dr. Tommaso Andreussi, Sitael Spa, Italy; Dr. Angela Rossodivita, Sitael Spa, Italy; Mr. Giorgio Saccoccia, European Space Agency (ESA), The Netherlands;
A 20KW-Class Hall Effect Thruster to Enhance Present and Future Space
published pages: , ISSN: , DOI:
69th International Astronautical Congress (IAC), 1-5 October 2018; IAC-18 2020-04-08
2017 Mariano Andrenucci (SITAEL)
Electric Propulsion: Gearing a Spacefaring Future
published pages: , ISSN: , DOI:
68th International Astronautical Congress (IAC), 25-29 September 2017 IAC-17 2020-04-08
2018 Dr. Julien Vaudolon, Safran Aircraft Engines, France; Dr. Vanessa Vial, Safran Aircraft Engines, France; Mr. Nicolas Cornu, Safran Aircraft Engines, France; Mr. Idris Habbassi, Safran Aircraft Engines, France;
PPS(R)X00 Hall Thruster Development at SAFRAN
published pages: , ISSN: , DOI:
69th International Astronautical Congress (IAC), 1-5 October 2018 IAC-18 2020-04-08
2017 Dr. Vanessa Vial, SAFRAN Aircraft Engines, France
ELECTRIC PROPULSION AT SAFRAN
published pages: , ISSN: , DOI:
68th International Astronautical Congress 2017 IAC-17 2020-04-08
2018 Birk Wollenhaupt (OHB)
FUTURE ELECTRIC PROPULSION NEEDS DEDUCED FROM LAUNCHER AND MISSION CONSTRAINTS
published pages: , ISSN: , DOI:
69th International Astronautical Congress (IAC), 1-5 October 2018 IAC-18 2020-04-08
2017 D. Pedrini (SITAEL) et. al.
Sitael Hollow Cathodes for Low-Power Hall Effect Thrusters
published pages: , ISSN: , DOI:
International Workshop on Micropropulsion and Cubesats MPCS-2017 2020-04-08
2018 Mr. Jorge LOPEZ REIG, CDTI (Centre for the development of Industrial Technology), Spain; Mr. Jose Gonzalez del Amo, European Space Agency (ESA), The Netherlands.
The Strategic Research Clusters on Space Electric Propulsion of the European Union’s Horizon 2020
published pages: , ISSN: , DOI:
69th International Astronautical Congress (IAC), 1-5 October 2018 IAC-18 2020-04-08
2017 E. Ahedo (UC3M)
Simulation Tools for Plasma Micro-Propulsion
published pages: , ISSN: , DOI:
international Workshop on Micropropulsion and Cubesats MPCS-2017 2020-04-08
2017 A. Domínguez, F. Cichocki, M. Merino, P. Fajardo and E. Ahedo
2D and 3D hybrid PIC- uid modeling of electric thruster plumes
published pages: 12, ISSN: , DOI:
IEPC Conference Proceeding 2017-209 2020-04-08
2017 S. Mazouffre, G. Largeau, L. Garrigues, C. Boniface, K. Dannenmayer
Evaluation of Various Probe Designs for Measuring the Ion Current Density in a Hall Thruster Plume
published pages: 17, ISSN: , DOI:
IEPC Conference Proceeding 2017-336 2020-04-08
2017 R. Lucken, V. Croes, T. Lafleur, J.-L. Raimbault, A. Bourdon and P. Chabert
Global models of plasma thrusters: Insights from PIC simulation and fluid theory
published pages: 15, ISSN: , DOI:
IEPC Conference Proceeding 2017-323 2020-04-08
2017 D. Pérez-Grande, J. Zhou, A. Domínguez, P. Fajardo and E. Ahedo
Development updates for a two- dimensional axisymmetric hybrid code for Plasma Thrusterdischarges
published pages: 19, ISSN: , DOI:
IEPC Conference Proceeding 2017-201 2020-04-08
2017 V. Croes, A. Tavant, R. Lucken, T. Lafleur, A. Bourdon and P. Chabert
Study of electron transport in a Hall effect thruster with 2D r-Θ Particle-In-Cell simulations
published pages: 15, ISSN: , DOI:
IEPC Conference Proceeding 2017-57 2020-04-08

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