HelIcon PlasmA Thruster for In-space Applications

Projektinformationen

HIPATIA

ID Finanzhilfevereinbarung: 870542

DOI 10.3030/870542

Projekt abgeschlossen

EK-Unterschriftsdatum 7 November 2019

Startdatum 1 Januar 2020

Enddatum 31 Dezember 2022

Finanziert unter

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

Gesamtkosten € 1 999 773,75

EU-Beitrag € 1 999 773,75

Koordiniert durch

SENER AEROESPACIAL SOCIEDAD ANONIMA
Spain

Leistungen

Other (1)

Peer-reviewed, conference and workshops publications

Peer-reviewed, conference and workshops publications. They will be issued at different times during the whole project duration.

Documents, reports (4)

HIPATIA Communication Plan

HIPATIA Communication Plan.

HIPATIA technology status assessment

HIPATIA technology status assessment.

Final HIPATIA Project Report
HIPATIA 1st Period Report

Websites, patent fillings, videos etc. (2)

HIPATIA website and social media profiles

HIPATIA website and social media profiles.

Communication material

Communication material. They will be issued at different times during the whole project duration.

Open Research Data Pilot (1)

Data Management Plan

Data Management PlanIt will be issued in M4 M12 M24 and M30There are different activities and deliverables in the Project that will make available open research data files specially Publications in conferentces and peer reviewed journals Datasets resulting from some of the activties devoted to simulation and testsThese datasets have not been appointed as independent deliverables in the deliverables lists They will be the open part of larger deliveries that will not be fully public

Veröffentlichungen

Thesis and dissertations (3)

DIAGNOSTIC METHODS FOR THE CHARACTERIZATION OF A HELICON PLASMA THRUSTER

Autoren: Mick Wijnen
Veröffentlicht in: 2023
Herausgeber: Universidad Carlos III de Madrid

Modeling and simulation of the plasma discharge in a radiofrequency thruster

Autoren: Zhou, Jiewei
Veröffentlicht in: instname:, Ausgabe 1, 2021
Herausgeber: Universidad Carlos III de Madrid

Physics of magnetic nozzles and helicon plasma discharges

Autoren: Alfio Vinci
Veröffentlicht in: 2022
Herausgeber: Institut de combustion aérothermique réactivité et environnement

Peer reviewed articles (10)

Magnetized fluid electron model within a two-dimensional hybrid simulation code for electrodeless plasma thrusters

Autoren: ZHOU, J.; DOMINGUEZ-VAZQUEZ, A.; FAJARDO, P.; AHEDO, E.
Veröffentlicht in: Plasma Sources Sciences and Technology, 2022, ISSN 0963-0252
Herausgeber: Institute of Physics Publishing
DOI: 10.1088/1361-6595/ac64bc

Direct experimental comparison of krypton and xenon discharge properties in the magnetic nozzle of a helicon plasma source

Autoren: Alfio E. Vinci, Stéphane Mazouffre
Veröffentlicht in: Physics of Plasmas, Ausgabe 28/3, 2021, Seite(n) 033504, ISSN 1070-664X
Herausgeber: American Institute of Physics
DOI: 10.1063/5.0037117

Plasma properties conditioned by the magnetic throat location in a helicon plasma device

Autoren: VINCI, A. E.; and MAZOUFFRE, S.
Veröffentlicht in: Journal of Applied Physics,, 2021, ISSN 0021-8979
Herausgeber: American Institute of Physics
DOI: 10.1063/5.0069983

Ion dynamics in the magnetic nozzle of a waveguide ECR thruster via laser-induced fluorescence spectroscopy

Autoren: VINCI, A. E.; M. R. INCHINGOLO; MAZOUFFRE, S.; NAVARRO-CAVALLÉ, J.
Veröffentlicht in: Phys. D: Appl. Phys., 2022, ISSN 0022-3727
Herausgeber: Institute of Physics Publishing
DOI: 10.1088/1361-6463/aca105

Mechanically Amplified Milli-Newton Thrust Balance for Direct Thrust Measurements of Electric Thrusters for Space Propulsion

Autoren: Mick Wijnen, Jaume Navarro-Cavalle, Pablo Fajardo
Veröffentlicht in: IEEE Transactions on Instrumentation and Measurement, Ausgabe 70, 2021, Seite(n) 1-18, ISSN 0018-9456
Herausgeber: Institute of Electrical and Electronics Engineers
DOI: 10.1109/tim.2020.3037305

Laser-induced fluorescence spectroscopy on xenon atoms and ions in the magnetic nozzle of a Helicon plasma thruster

Autoren: VINCI, A. E.; MAZOUFFRE, S.; GÓMEZ, V.; FAJARDO, P.; NAVARRO-CAVALLÉ, J.
Veröffentlicht in: Plasma Sources Science and Technology, 2023, ISSN 0963-0252
Herausgeber: Institute of Physics Publishing
DOI: 10.1088/1361-6595/ac8db8

Enhanced electron heating in the magnetic nozzle of a radio-frequency plasma via electron cyclotron resonance

Autoren: VINCI, A. E.; MAZOUFFRE, S.;
Veröffentlicht in: Eur. Phys. Lett., 2023, ISSN 0295-5075
Herausgeber: EDP Sciences
DOI: 10.1209/0295-5075/acb967

Magnetic Nozzle and RPA Simulations vs. Experiments for a Helicon Plasma Thruster Plume

Autoren: Filippo Cichocki; Jaume Navarro-Cavallé; Alberto Modesti; Gonzalo Ramírez Vázquez
Veröffentlicht in: Frontiers in Physics 10 (2022): 876684-1–876684-15. doi:10.3389/fphy.2022.876684, Ausgabe 2, 2022, ISSN 2296-424X
Herausgeber: Frontiers
DOI: 10.3389/fphy.2022.876684

Wave propagation and absorption in a helicon plasma thruster and its plume

Autoren: PEDRO JIMENEZ; EDUARDO AHEDO; Mario Merino
Veröffentlicht in: Crossref, Ausgabe 3, 2022, ISSN 0963-0252
Herausgeber: Institute of Physics Publishing
DOI: 10.1088/1361-6595/ac5ecd

Electron thermodynamics along magnetic nozzle lines in a helicon plasma

Autoren: Alfio E. Vinci; Quentin Delavière–Delion; Stéphane Mazouffre
Veröffentlicht in: Journal of Electric Propulsion, Ausgabe 1, 2022, ISSN 2731-4596
Herausgeber: Springer
DOI: 10.1007/s44205-022-00003-0

Conference proceedings (6)

HIPATIA: A project for the development of the Helicon Plasma Thruster and its associated technologies to intermediate-high TRLs

Autoren: Ruiz, Mercedes; Gómez, V; Fajardo, P; Navarro, J; Albertoni, R; Dickeli, G; Vinci, A; Mazouffre, Stéphane; Hildebrand, N
Veröffentlicht in: https://hal.archives-ouvertes.fr/hal-02995461, Ausgabe 1, 2020
Herausgeber: IAC

Electron and Ion Properties in the Beam and Discharge of a Helicon Plasma Source for Application in Spacecraft Propulsion

Autoren: VINCI, A. E.; MAZOUFFRE, S.
Veröffentlicht in: Space Propulsion Conference, virtual conference, 2021
Herausgeber: Association Aéronautique et Astronautique de France

The Hipatia project´s initial development stages: setting the basis to bring the Helicon Plasma Thruster and its associated technologies to intermediate-high TRLs

Autoren: RUIZ, M.; GÓMEZ, V.; FAJARDO, P.; NAVARRO, J.; ALBERTONI, R.; DICKELI, G.; VINCI, A.; MAZOUFFRE, S.; and HILDEBRAND, N.
Veröffentlicht in: 7th Space Propulsion Conference, virtual conference,, 2021
Herausgeber: Association Aéronautique et Astronautique de France

Performance analysis of alternative propellants for a helicon plasma thruster

Autoren: ZHOU, J.; TACCOGNA, F.; FAJARDO, P.; and AHEDO, E
Veröffentlicht in: 7th Space Propulsion Conference, vitual conference,, 2021
Herausgeber: Association Aéronautique et Astronautique de France

Preliminary investigation of the electromagnetic fields in the plume of a Helicon Plasma Thruster

Autoren: JIMENEZ, P.; MERINO, M.; and AHEDO, E.
Veröffentlicht in: 7th Space Propulsion Conference, virtual conference, 2021, 2021
Herausgeber: Association Aéronautique et Astronautique de France

Performance analysis of alternative propellants for a helicon plasma thruster

Autoren: ZHOU, J.; TACCOGNA, F.; FAJARDO, P.; and AHEDO, E
Veröffentlicht in: 7th Space Propulsion Conference, vitual conference, 2021
Herausgeber: Association Aéronautique et Astronautique de France