Explore the words cloud of the CHEOPS project. It provides you a very rough idea of what is the project "CHEOPS" about.
The following table provides information about the project.
Coordinator |
SAFRAN AIRCRAFT ENGINES
Organization address contact info |
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 |
Take a look of project's partnership.
# | ||||
---|---|---|---|---|
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 |
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.
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.
year | authors and title | journal | last update |
---|---|---|---|
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. DomÃnguez, 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. DomÃnguez, 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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