Consortium for Hall Effect Orbital Propulsion System

Project Information

CHEOPS

Grant agreement ID: 730135

DOI 10.3030/730135

Project closed

EC signature date 24 October 2016

Start date 1 November 2016

End date 30 April 2021

Funded under

• INDUSTRIAL LEADERSHIP - Leadership in enabling and industrial technologies – Space

Total cost € 14 792 359,43

EU contribution € 10 960 028,89

Coordinated by

SAFRAN SPACECRAFT PROPULSION
France

Deliverables

Documents, reports (6)

Dissemination report ed2

-List of dissemination initiative by each partner and update of dissemination plan

E-T System test report

Posttest data analysis on high power system test

Guide for value, cost and functional modelling

A guide for partners to use when contributing to value, cost and functional modelling of the different propulsion designs studied.

Dissemination report ed1

List of dissemination initiative by each partner and update of dissemination plan

Value Creation Strategy (Collective Value Creation Strategies

A consolidated report on the expected value and cost - competitive profile (VCS) for the different propulsion systems, including the relative base line system(s) for comparison.

Dissemination report Final

Final dissemination report including all dissemination activities

Websites, patent fillings, videos etc. (1)

CHEOPS public website

S4S will be responsible for the project’s public web-site development and maintenance, using it to describe the systems and the work, and providing access to the open publications, presentations, poster/s, brochure/s, etc. regarding the project;

Publications

Conference proceedings (24)

Development of High-Current Hollow Cathodes at SITAEL

Author(s): A. Kitaeva et al.
Published in: 71st International Astronautical Congress (IAC), Issue IAC-20, 2020
Publisher: IAC CyberSpace Edition

NOMADS: DEVELOPMENT OF A VERSATILE PLASMA DISCHARGE SIMULATION PLATFORM FOR ELECTRIC PROPULSION.

Author(s): Domínguez, A., et al.
Published in: Space Propulsion Conference Proceedings, Issue SP 2016, 2016
Publisher: Space Propulsion Conference

design optimization and development status of electric propulsion system for satellites

Author(s): Vanessa Vial, Vincent Guyon, Frédéric Marchandise, Michael Öberg
Published in: 72nd International Astronautical Congress (IAC), Issue IAC 2021, 2021
Publisher: IAF

Development Status of SITAEL’s 20 kW Class Hall Thruster

Author(s): Antonio Piragino et al.
Published in: AIAA Propulsion and Energy 2019 Forum, Issue AIAA 2019-3812, 2019
Publisher: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2019-3812

Analysis of plasma discharge in HET via hybrid 2D code

Author(s): Domínguez et al.
Published in: IEPC Conference Proceeding, Issue IEPC 2019-579, 2019
Publisher: University of Vienna

Development status and way forward of SITAEL's 20kW class Hall thruster, the HT20k

Author(s): Tommaso Andreussi, et al.
Published in: IEPC Conference Proceeding, Issue IEPC 2019-825, 2019
Publisher: University of Vienna

extended qualification life test of the PPS®5000 hall thruster unit, ,

Author(s): Vanessa Vial, Olivier Duchemin, Giovanni Codutti, David Le Méhauté, Julien Rabin
Published in: 72nd International Astronautical Congress (IAC), Issue IAC 2021, 2021
Publisher: IAF

Evaluation of Various Probe Designs for Measuring the Ion Current Density in a Hall Thruster Plume

Author(s): S. Mazouffre, G. Largeau, L. Garrigues, C. Boniface, K. Dannenmayer
Published in: IEPC Conference Proceeding, Issue 2017-336, 2017, Page(s) 17
Publisher: Electric Rocket Propulsion Society

Global models of plasma thrusters: Insights from PIC simulation and fluid theory

Author(s): R. Lucken, V. Croes, T. Lafleur, J.-L. Raimbault, A. Bourdon and P. Chabert
Published in: IEPC Conference Proceeding, Issue 2017-323, 2017, Page(s) 15
Publisher: Electric Rocket Propulsion Society

2D and 3D hybrid PIC- uid modeling of electric thruster plumes

Author(s): A. Domínguez, F. Cichocki, M. Merino, P. Fajardo and E. Ahedo
Published in: IEPC Conference Proceeding, Issue 2017-209, 2017, Page(s) 12
Publisher: Electric Rocket Propulsion Society

Study of electron transport in a Hall effect thruster with 2D r-Θ Particle-In-Cell simulations

Author(s): V. Croes, A. Tavant, R. Lucken, T. Lafleur, A. Bourdon and P. Chabert
Published in: IEPC Conference Proceeding, Issue 2017-57, 2017, Page(s) 15
Publisher: Electric Rocket Propulsion Society

Development updates for a two- dimensional axisymmetric hybrid code for Plasma Thrusterdischarges

Author(s): D. Pérez-Grande, J. Zhou, A. Domínguez, P. Fajardo and E. Ahedo
Published in: IEPC Conference Proceeding, Issue 2017-201, 2017, Page(s) 19
Publisher: Electric Rocket Propulsion Society

HT20k Hall Thruster development status

Author(s): Tommaso Andreussi, Antonio Piragino, Eugenio Ferrato, Maryam Reza, Farbod Faraji, Giulia Becatti, Daniela Pedrini, Alena Kitaeva, Angela Rossodivita, Mariano Andrenucci
Published in: 69th International Astronautical Congress (IAC), Bremen, Germany, 1-5 October 2018., Issue IAC-18, 2018
Publisher: IAF

Power Processing Unit Activites at Thales Alenia Space in Belgium

Author(s): Eric Bourguignon, Stéphane Fraselle
Published in: Space Propulsion Conference Proceedings, Issue SP 2018, 2018
Publisher: Space Propulsion

PPU Mk3 for 5 kW Hall Effect Thrusters

Author(s): Eric Bourguignon, Stéphane Fraselle
Published in: IEPC Conference Proceeding, Issue 2017-171, 2017
Publisher: IEPC

PPS(R)X00 Hall Thruster Development at SAFRAN

Author(s): 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;
Published in: 69th International Astronautical Congress (IAC), 1-5 October 2018, Issue IAC-18, 2018
Publisher: IAF

A 20KW-Class Hall Effect Thruster to Enhance Present and Future Space

Author(s): 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;
Published in: 69th International Astronautical Congress (IAC), 1-5 October 2018;, Issue IAC-18, 2018
Publisher: IAF

FUTURE ELECTRIC PROPULSION NEEDS DEDUCED FROM LAUNCHER AND MISSION CONSTRAINTS

Author(s): Birk Wollenhaupt (OHB)
Published in: 69th International Astronautical Congress (IAC), 1-5 October 2018, Issue IAC-18, 2018
Publisher: IAF

Sitael Hollow Cathodes for Low-Power Hall Effect Thrusters

Author(s): D. Pedrini (SITAEL) et. al.
Published in: International Workshop on Micropropulsion and Cubesats, Issue MPCS-2017, 2017
Publisher: CNR-Nanotec

Simulation Tools for Plasma Micro-Propulsion

Author(s): E. Ahedo (UC3M)
Published in: international Workshop on Micropropulsion and Cubesats, Issue MPCS-2017, 2017
Publisher: CNR-Nanotec

The Strategic Research Clusters on Space Electric Propulsion of the European Union’s Horizon 2020

Author(s): Mr. Jorge LOPEZ REIG, CDTI (Centre for the development of Industrial Technology), Spain; Mr. Jose Gonzalez del Amo, European Space Agency (ESA), The Netherlands.
Published in: 69th International Astronautical Congress (IAC), 1-5 October 2018, Issue IAC-18, 2018
Publisher: IAF

Electric Propulsion: Gearing a Spacefaring Future

Author(s): Mariano Andrenucci (SITAEL)
Published in: 68th International Astronautical Congress (IAC), 25-29 September 2017, Issue IAC-17, 2017
Publisher: IAF

ELECTRIC PROPULSION AT SAFRAN

Author(s): Dr. Vanessa Vial, SAFRAN Aircraft Engines, France
Published in: 68th International Astronautical Congress 2017, Issue IAC-17, 2017
Publisher: IAF

PPS®X00 Hall Thruster Development status, ,

Author(s): Vanessa Vial, Anthony Caron, Alberto Alonso Gonzalez, Claude-Martin Brito
Published in: 72nd International Astronautical Congress (IAC), Issue IAC 2021, 2021
Publisher: IAF

Peer reviewed articles (3)

Particle modelling of radial electron dynamics in a controlled discharge of a Hall thruster

Author(s): A Domínguez-Vázquez, F Taccogna and E Ahedo
Published in: Plasma Sources Science and Technology, Issue Volume 27, Number 6, 2018, ISSN 1361-6595
Publisher: IOP Publishing Ltd
DOI: 10.1088/1361-6595/aac968

Axisymmetric plasma plume characterization with 2D and 3D particle codes

Author(s): A Domínguez-Vázquez, F Cichocki, M Merino, P Fajardo and E Ahedo
Published in: Plasma Sources Science and Technology, Issue Volume 27, Number 10, 2018, ISSN 1361-6595
Publisher: IOP Publishing Ltd
DOI: 10.1088/1361-6595/aae702

Parametric study of the radial plasma-wall interaction in a Hall thruster

Author(s): A Domínguez-Vázquez, F Taccogna, P Fajardo and E Ahedo
Published in: Journal of Physics D: Applied Physics, Issue Volume 52, Number 47, 2019, ISSN 1361-6463
Publisher: IOP Publishing Ltd
DOI: 10.1088/1361-6463/ab3c7b