Zobrazeno 1 - 10
of 22
pro vyhledávání: '"Gurciullo, Antonio"'
Autor:
Koopmans, Robert-Jan, Białek, Agata, Donohoe, Anthony, Jiménez, María Fernández, Frasl, Barbara, Gurciullo, Antonio, Kleinschneider, Andreas, Łosiak, Anna, Mannel, Thurid, Elorza, Iñigo Muñoz, Nilsson, Daniel, Oliveira, Marta, Sørensen-Clark, Paul Magnus, Timoney, Ryan, van Zelst, Iris
The Hesperos mission proposed in this paper is a mission to Venus to investigate the interior structure and the current level of activity. The main questions to be answered with this mission are whether Venus has an internal structure and composition
Externí odkaz:
http://arxiv.org/abs/1803.06652
Autor:
Gurciullo, Antonio
There are open issues within the uctuation theory owing to the approximations invoked in regimes outside fully ionized collisionless plasmas. This includes laboratory and space environments where e ects of Coulomb collisions or collisions with neutra
Externí odkaz:
http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-170436
Publikováno v:
In Acta Astronautica September 2020 174:219-235
Autor:
Lascombes, Paul, Montès, Maxime, Fiorentino, Andrea, Gelu, Tom, Fillastre, Mikael, Gurciullo, Antonio
Publikováno v:
Small Satellite Conference
Only a few electric propulsion solutions on-board small satellites have been operated in space, even if propulsion is nowadays seen as one of the most important subsystems for the future of small satellites. Exotrail demonstrated its Hall Effect Thru
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______1459::39b457ea5eda7fbff6c0610266fdf06b
https://digitalcommons.usu.edu/smallsat/2021/all2021/204
https://digitalcommons.usu.edu/smallsat/2021/all2021/204
Autor:
Gurciullo, Antonio
The focus of this research is to explore technologies for enabling the use of molecular propellants in the �field of electric propulsion. The research presented in this thesis addresses three main areas of development: plasma physics modelling of h
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::b866c74f686aa0047847797eb2556579
Publikováno v:
IEPC 2019
IEPC 2019, Sep 2019, VIENNE, Austria
IEPC 2019, Sep 2019, VIENNE, Austria
International audience; The performance metrics and the plume characteristics of a miniaturised Hall thruster are investigated. The thruster is part of the ExoMG-nano propulsion platform developed by Exotrail and, during the test campaign, it is oper
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______2592::94d6825607500da8a7ac197175124db9
https://hal.archives-ouvertes.fr/hal-02422774/file/DPHY19105.1576242677.pdf
https://hal.archives-ouvertes.fr/hal-02422774/file/DPHY19105.1576242677.pdf
Publikováno v:
IEPC 2019
IEPC 2019, Sep 2019, VIENNE, Austria
IEPC 2019, Sep 2019, VIENNE, Austria
International audience; The performance metrics and the plume characteristics of a miniaturised Hall thruster are investigated. The thruster is part of the ExoMG-nano propulsion platform developed by Exotrail and, during the test campaign, it is oper
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::94d6825607500da8a7ac197175124db9
https://hal.archives-ouvertes.fr/hal-02422774/file/DPHY19105.1576242677.pdf
https://hal.archives-ouvertes.fr/hal-02422774/file/DPHY19105.1576242677.pdf
The ion plume of a 72mm diameter Hall Effect Thruster operated on mixtures of xenon/nitrogen and xenon/air is investigated by means of a Wien filter (or E x B probe). The dependence of the velocities of the plume ions (Xe⁺, Xe²⁺, Xe³⁺, O₂
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od_______305::309258e5a45f23b9797b1fe0690010ff
https://surrey.eprints-hosting.org/852462/
https://surrey.eprints-hosting.org/852462/
Autor:
Mazouffre, Stéphane, Hallouin, Thibault, Inchingolo, Marco, Gurciullo, Antonio, Lascombes, Paul, Maria, Jean-Luc
After a brief introduction to micropropulsion devices for small spacecraft and low-power Hall thruster performances in terms of thrust and specific impulse, this study focuses on plasma plume properties. The plume of the 100 W-class ISCT100-v2 Hall t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::2e95e86cc8ec4872431a7b77a6e0b154
Autor:
Lucca Fabris, Andrea, Wantock, Tom, Gurciullo, Antonio, Moloney, Rachel, Knoll, A., Potterton, T., Bianco, P.
The Halo thruster is a low-power plasma propulsion concept, currently under investigation and development within the Surrey Space Centre at the University of Surrey in collaboration with Surrey Satellite Technology Ltd, Airbus DS and Imperial College
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od_______305::0deda834de90e8cf33295712b0337125
https://surrey.eprints-hosting.org/850112/
https://surrey.eprints-hosting.org/850112/