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Consortium for Hall Effect Orbital Propulsion System

Risultati finali

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;

Pubblicazioni

Development of High-Current Hollow Cathodes at SITAEL

Autori: A. Kitaeva et al.
Pubblicato in: 71st International Astronautical Congress (IAC), IAC-20, 2020
Editore: IAC CyberSpace Edition

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

Autori: Domínguez, A., et al.
Pubblicato in: Space Propulsion Conference Proceedings, SP 2016, 2016
Editore: Space Propulsion Conference

design optimization and development status of electric propulsion system for satellites

Autori: Vanessa Vial, Vincent Guyon, Frédéric Marchandise, Michael Öberg
Pubblicato in: 72nd International Astronautical Congress (IAC), IAC 2021, 2021
Editore: IAF

Development Status of SITAEL’s 20 kW Class Hall Thruster

Autori: Antonio Piragino et al.
Pubblicato in: AIAA Propulsion and Energy 2019 Forum, AIAA 2019-3812, 2019
Editore: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2019-3812

Analysis of plasma discharge in HET via hybrid 2D code

Autori: Domínguez et al.
Pubblicato in: IEPC Conference Proceeding, IEPC 2019-579, 2019
Editore: University of Vienna

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

Autori: Tommaso Andreussi, et al.
Pubblicato in: IEPC Conference Proceeding, IEPC 2019-825, 2019
Editore: University of Vienna

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

Autori: Vanessa Vial, Olivier Duchemin, Giovanni Codutti, David Le Méhauté, Julien Rabin
Pubblicato in: 72nd International Astronautical Congress (IAC), IAC 2021, 2021
Editore: IAF

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

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

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

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

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

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

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

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

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

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

HT20k Hall Thruster development status

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

Power Processing Unit Activites at Thales Alenia Space in Belgium

Autori: Eric Bourguignon, Stéphane Fraselle
Pubblicato in: Space Propulsion Conference Proceedings, SP 2018, 2018
Editore: Space Propulsion

PPU Mk3 for 5 kW Hall Effect Thrusters

Autori: Eric Bourguignon, Stéphane Fraselle
Pubblicato in: IEPC Conference Proceeding, 2017-171, 2017
Editore: IEPC

PPS(R)X00 Hall Thruster Development at SAFRAN

Autori: 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;
Pubblicato in: 69th International Astronautical Congress (IAC), 1-5 October 2018, IAC-18, 2018
Editore: IAF

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

Autori: 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;
Pubblicato in: 69th International Astronautical Congress (IAC), 1-5 October 2018;, IAC-18, 2018
Editore: IAF

FUTURE ELECTRIC PROPULSION NEEDS DEDUCED FROM LAUNCHER AND MISSION CONSTRAINTS

Autori: Birk Wollenhaupt (OHB)
Pubblicato in: 69th International Astronautical Congress (IAC), 1-5 October 2018, IAC-18, 2018
Editore: IAF

Sitael Hollow Cathodes for Low-Power Hall Effect Thrusters

Autori: D. Pedrini (SITAEL) et. al.
Pubblicato in: International Workshop on Micropropulsion and Cubesats, MPCS-2017, 2017
Editore: CNR-Nanotec

Simulation Tools for Plasma Micro-Propulsion

Autori: E. Ahedo (UC3M)
Pubblicato in: international Workshop on Micropropulsion and Cubesats, MPCS-2017, 2017
Editore: CNR-Nanotec

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

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

Electric Propulsion: Gearing a Spacefaring Future

Autori: Mariano Andrenucci (SITAEL)
Pubblicato in: 68th International Astronautical Congress (IAC), 25-29 September 2017, IAC-17, 2017
Editore: IAF

ELECTRIC PROPULSION AT SAFRAN

Autori: Dr. Vanessa Vial, SAFRAN Aircraft Engines, France
Pubblicato in: 68th International Astronautical Congress 2017, IAC-17, 2017
Editore: IAF

PPS®X00 Hall Thruster Development status, ,

Autori: Vanessa Vial, Anthony Caron, Alberto Alonso Gonzalez, Claude-Martin Brito
Pubblicato in: 72nd International Astronautical Congress (IAC), IAC 2021, 2021
Editore: IAF

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

Autori: A Domínguez-Vázquez, F Taccogna and E Ahedo
Pubblicato in: Plasma Sources Science and Technology, Volume 27, Number 6, 2018, ISSN 1361-6595
Editore: IOP Publishing Ltd
DOI: 10.1088/1361-6595/aac968

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

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

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

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