Consortium for Hall Effect Orbital Propulsion System

Rezultaty

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

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;

Publikacje

Development of High-Current Hollow Cathodes at SITAEL

Autorzy: A. Kitaeva et al.
Opublikowane w: 71st International Astronautical Congress (IAC), IAC-20, 2020
Wydawca: IAC CyberSpace Edition

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

Autorzy: Domínguez, A., et al.
Opublikowane w: Space Propulsion Conference Proceedings, SP 2016, 2016
Wydawca: Space Propulsion Conference

design optimization and development status of electric propulsion system for satellites

Autorzy: Vanessa Vial, Vincent Guyon, Frédéric Marchandise, Michael Öberg
Opublikowane w: 72nd International Astronautical Congress (IAC), IAC 2021, 2021
Wydawca: IAF

Development Status of SITAEL’s 20 kW Class Hall Thruster

Autorzy: Antonio Piragino et al.
Opublikowane w: AIAA Propulsion and Energy 2019 Forum, AIAA 2019-3812, 2019
Wydawca: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2019-3812

Analysis of plasma discharge in HET via hybrid 2D code

Autorzy: Domínguez et al.
Opublikowane w: IEPC Conference Proceeding, IEPC 2019-579, 2019
Wydawca: University of Vienna

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

Autorzy: Tommaso Andreussi, et al.
Opublikowane w: IEPC Conference Proceeding, IEPC 2019-825, 2019
Wydawca: University of Vienna

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

Autorzy: Vanessa Vial, Olivier Duchemin, Giovanni Codutti, David Le Méhauté, Julien Rabin
Opublikowane w: 72nd International Astronautical Congress (IAC), IAC 2021, 2021
Wydawca: IAF

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

Autorzy: S. Mazouffre, G. Largeau, L. Garrigues, C. Boniface, K. Dannenmayer
Opublikowane w: IEPC Conference Proceeding, 2017-336, 2017, Page(s) 17
Wydawca: Electric Rocket Propulsion Society

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

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

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

Autorzy: A. Domínguez, F. Cichocki, M. Merino, P. Fajardo and E. Ahedo
Opublikowane w: IEPC Conference Proceeding, 2017-209, 2017, Page(s) 12
Wydawca: Electric Rocket Propulsion Society

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

Autorzy: V. Croes, A. Tavant, R. Lucken, T. Lafleur, A. Bourdon and P. Chabert
Opublikowane w: IEPC Conference Proceeding, 2017-57, 2017, Page(s) 15
Wydawca: Electric Rocket Propulsion Society

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

Autorzy: D. Pérez-Grande, J. Zhou, A. Domínguez, P. Fajardo and E. Ahedo
Opublikowane w: IEPC Conference Proceeding, 2017-201, 2017, Page(s) 19
Wydawca: Electric Rocket Propulsion Society

HT20k Hall Thruster development status

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

Power Processing Unit Activites at Thales Alenia Space in Belgium

Autorzy: Eric Bourguignon, Stéphane Fraselle
Opublikowane w: Space Propulsion Conference Proceedings, SP 2018, 2018
Wydawca: Space Propulsion

PPU Mk3 for 5 kW Hall Effect Thrusters

Autorzy: Eric Bourguignon, Stéphane Fraselle
Opublikowane w: IEPC Conference Proceeding, 2017-171, 2017
Wydawca: IEPC

PPS(R)X00 Hall Thruster Development at SAFRAN

Autorzy: 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;
Opublikowane w: 69th International Astronautical Congress (IAC), 1-5 October 2018, IAC-18, 2018
Wydawca: IAF

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

Autorzy: 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;
Opublikowane w: 69th International Astronautical Congress (IAC), 1-5 October 2018;, IAC-18, 2018
Wydawca: IAF

FUTURE ELECTRIC PROPULSION NEEDS DEDUCED FROM LAUNCHER AND MISSION CONSTRAINTS

Autorzy: Birk Wollenhaupt (OHB)
Opublikowane w: 69th International Astronautical Congress (IAC), 1-5 October 2018, IAC-18, 2018
Wydawca: IAF

Sitael Hollow Cathodes for Low-Power Hall Effect Thrusters

Autorzy: D. Pedrini (SITAEL) et. al.
Opublikowane w: International Workshop on Micropropulsion and Cubesats, MPCS-2017, 2017
Wydawca: CNR-Nanotec

Simulation Tools for Plasma Micro-Propulsion

Autorzy: E. Ahedo (UC3M)
Opublikowane w: international Workshop on Micropropulsion and Cubesats, MPCS-2017, 2017
Wydawca: CNR-Nanotec

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

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

Electric Propulsion: Gearing a Spacefaring Future

Autorzy: Mariano Andrenucci (SITAEL)
Opublikowane w: 68th International Astronautical Congress (IAC), 25-29 September 2017, IAC-17, 2017
Wydawca: IAF

ELECTRIC PROPULSION AT SAFRAN

Autorzy: Dr. Vanessa Vial, SAFRAN Aircraft Engines, France
Opublikowane w: 68th International Astronautical Congress 2017, IAC-17, 2017
Wydawca: IAF

PPS®X00 Hall Thruster Development status, ,

Autorzy: Vanessa Vial, Anthony Caron, Alberto Alonso Gonzalez, Claude-Martin Brito
Opublikowane w: 72nd International Astronautical Congress (IAC), IAC 2021, 2021
Wydawca: IAF

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

Autorzy: A Domínguez-Vázquez, F Taccogna and E Ahedo
Opublikowane w: Plasma Sources Science and Technology, Volume 27, Number 6, 2018, ISSN 1361-6595
Wydawca: IOP Publishing Ltd
DOI: 10.1088/1361-6595/aac968

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

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

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

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

Rezultaty

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