Skip to main content

Consortium for Hall Effect Orbital Propulsion System

Resultado final

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

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;

Publicaciones

Development of High-Current Hollow Cathodes at SITAEL

Autores: A. Kitaeva et al.
Publicado en: 71st International Astronautical Congress (IAC), IAC-20, 2020
Editor: IAC CyberSpace Edition

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

Autores: Domínguez, A., et al.
Publicado en: Space Propulsion Conference Proceedings, SP 2016, 2016
Editor: Space Propulsion Conference

design optimization and development status of electric propulsion system for satellites

Autores: Vanessa Vial, Vincent Guyon, Frédéric Marchandise, Michael Öberg
Publicado en: 72nd International Astronautical Congress (IAC), IAC 2021, 2021
Editor: IAF

Development Status of SITAEL’s 20 kW Class Hall Thruster

Autores: Antonio Piragino et al.
Publicado en: AIAA Propulsion and Energy 2019 Forum, AIAA 2019-3812, 2019
Editor: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2019-3812

Analysis of plasma discharge in HET via hybrid 2D code

Autores: Domínguez et al.
Publicado en: IEPC Conference Proceeding, IEPC 2019-579, 2019
Editor: University of Vienna

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

Autores: Tommaso Andreussi, et al.
Publicado en: IEPC Conference Proceeding, IEPC 2019-825, 2019
Editor: University of Vienna

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

Autores: Vanessa Vial, Olivier Duchemin, Giovanni Codutti, David Le Méhauté, Julien Rabin
Publicado en: 72nd International Astronautical Congress (IAC), IAC 2021, 2021
Editor: IAF

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

Autores: S. Mazouffre, G. Largeau, L. Garrigues, C. Boniface, K. Dannenmayer
Publicado en: IEPC Conference Proceeding, 2017-336, 2017, Page(s) 17
Editor: Electric Rocket Propulsion Society

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

Autores: R. Lucken, V. Croes, T. Lafleur, J.-L. Raimbault, A. Bourdon and P. Chabert
Publicado en: IEPC Conference Proceeding, 2017-323, 2017, Page(s) 15
Editor: Electric Rocket Propulsion Society

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

Autores: A. Domínguez, F. Cichocki, M. Merino, P. Fajardo and E. Ahedo
Publicado en: IEPC Conference Proceeding, 2017-209, 2017, Page(s) 12
Editor: Electric Rocket Propulsion Society

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

Autores: V. Croes, A. Tavant, R. Lucken, T. Lafleur, A. Bourdon and P. Chabert
Publicado en: IEPC Conference Proceeding, 2017-57, 2017, Page(s) 15
Editor: Electric Rocket Propulsion Society

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

Autores: D. Pérez-Grande, J. Zhou, A. Domínguez, P. Fajardo and E. Ahedo
Publicado en: IEPC Conference Proceeding, 2017-201, 2017, Page(s) 19
Editor: Electric Rocket Propulsion Society

HT20k Hall Thruster development status

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

Power Processing Unit Activites at Thales Alenia Space in Belgium

Autores: Eric Bourguignon, Stéphane Fraselle
Publicado en: Space Propulsion Conference Proceedings, SP 2018, 2018
Editor: Space Propulsion

PPU Mk3 for 5 kW Hall Effect Thrusters

Autores: Eric Bourguignon, Stéphane Fraselle
Publicado en: IEPC Conference Proceeding, 2017-171, 2017
Editor: IEPC

PPS(R)X00 Hall Thruster Development at SAFRAN

Autores: 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;
Publicado en: 69th International Astronautical Congress (IAC), 1-5 October 2018, IAC-18, 2018
Editor: IAF

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

Autores: 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;
Publicado en: 69th International Astronautical Congress (IAC), 1-5 October 2018;, IAC-18, 2018
Editor: IAF

FUTURE ELECTRIC PROPULSION NEEDS DEDUCED FROM LAUNCHER AND MISSION CONSTRAINTS

Autores: Birk Wollenhaupt (OHB)
Publicado en: 69th International Astronautical Congress (IAC), 1-5 October 2018, IAC-18, 2018
Editor: IAF

Sitael Hollow Cathodes for Low-Power Hall Effect Thrusters

Autores: D. Pedrini (SITAEL) et. al.
Publicado en: International Workshop on Micropropulsion and Cubesats, MPCS-2017, 2017
Editor: CNR-Nanotec

Simulation Tools for Plasma Micro-Propulsion

Autores: E. Ahedo (UC3M)
Publicado en: international Workshop on Micropropulsion and Cubesats, MPCS-2017, 2017
Editor: CNR-Nanotec

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

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

Electric Propulsion: Gearing a Spacefaring Future

Autores: Mariano Andrenucci (SITAEL)
Publicado en: 68th International Astronautical Congress (IAC), 25-29 September 2017, IAC-17, 2017
Editor: IAF

ELECTRIC PROPULSION AT SAFRAN

Autores: Dr. Vanessa Vial, SAFRAN Aircraft Engines, France
Publicado en: 68th International Astronautical Congress 2017, IAC-17, 2017
Editor: IAF

PPS®X00 Hall Thruster Development status, ,

Autores: Vanessa Vial, Anthony Caron, Alberto Alonso Gonzalez, Claude-Martin Brito
Publicado en: 72nd International Astronautical Congress (IAC), IAC 2021, 2021
Editor: IAF

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

Autores: A Domínguez-Vázquez, F Taccogna and E Ahedo
Publicado en: Plasma Sources Science and Technology, Volume 27, Number 6, 2018, ISSN 1361-6595
Editor: IOP Publishing Ltd
DOI: 10.1088/1361-6595/aac968

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

Autores: A Domínguez-Vázquez, F Cichocki, M Merino, P Fajardo and E Ahedo
Publicado en: Plasma Sources Science and Technology, Volume 27, Number 10, 2018, ISSN 1361-6595
Editor: IOP Publishing Ltd
DOI: 10.1088/1361-6595/aae702

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

Autores: A Domínguez-Vázquez, F Taccogna, P Fajardo and E Ahedo
Publicado en: Journal of Physics D: Applied Physics, Volume 52, Number 47, 2019, ISSN 1361-6463
Editor: IOP Publishing Ltd
DOI: 10.1088/1361-6463/ab3c7b