Zobrazeno 1 - 10 of 12 pro vyhledávání: '"Franco Javier Bosi"'
1
One-Dimensional Model for Hollow Cathode Orifice Lifetime Prediction
Autor: Franco Javier Bosi, Stephen Gabriel, Francesco Guarducci
Publikováno v: Journal of Propulsion and Power. 37:509-516
Lifetime assessment of hollow cathode (HC) sources is an experimentally demanding process, due to the large amount of hours space qualification requires. In this Paper, we present a one-dimensional...
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::1c2c6399b03060ca09ec00088270271c
https://doi.org/10.2514/1.b38094
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2
Numerical Suite for Gaseous Plasma Antennas Simulation
Autor: Franco Javier Bosi, Daniele Pavarin, Paola De Carlo, Antonio-D. Capobianco, Giulia Mansutti, Mirko Magarotto, Nicholas E. Buris
Publikováno v: IEEE Transactions on Plasma Science
A gaseous plasma antenna (GPA) is a device in which a plasma medium is used to transmit or receive electromagnetic (EM) waves. This work is devoted to the presentation of a numerical suite for the simulation of a GPA that consists of a plasma module
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::f615518ca3b0bf10a6c30ccf2167b5ae
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3
Global model of microwave plasma assisted N2O dissociation for monopropellant propulsion
Autor: Franco Javier Bosi
Publikováno v: Physics of Plasmas. 26:033510
A global numerical model is developed to study the capability of a Microwave Electro-thermal thruster (MET) to operate with Nitrous Oxide gas (N2O), for spacecraft monopropellant thruster applications. N2O is a “green” propellant with interesting
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::1d63eef9b810d73374424a12c9dee828
https://doi.org/10.1063/1.5066324
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4
Removal of persistent organic pollutants from water using a newly developed atmospheric plasma reactor
Autor: Alice Pavanello, Ester Marotta, Cristina Paradisi, Agata Giardina, Gabriele Neretti, Franco Javier Bosi, Barbara Zaniol, Francesco Tampieri
Publikováno v: Plasma Processes and Polymers. 15:1700207
A new bench-top reactor employing a streamer discharge in air was developed and tested for potential use in an advanced oxidation stage in water treatment processes. The complex heterogeneous system and the ensuing chemical processes were characteriz
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::8d9f546d9ad44a56ed6d79e95d43f762
https://doi.org/10.1002/ppap.201700207
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6
Modelling and Optimization of Electrode-less Helicon Plasma Thruster with Different Propellants
Autor: Davide Melazzi, Andrea Lucca Fabris, Marco Manente, Daniele Pavarin, Franco Javier Bosi, Fabio Trezzolani
Publikováno v: 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference.
In the framework of the ”Helicon Plasma Thruster for Space Missions AO7048” research program, a zero-dimensional numerical model is developed in order to assess the propulsive performances of the plasma thruster when fed with different molecular
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::e82d412f6cfb9b7b2428e52526c9b394
https://doi.org/10.2514/6.2014-3404
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7
Integrated Design Tools for RF Antennas for Helicon Plasma Thrusters
Autor: Vito Lancellotti, Daniele Pavarin, Fabio Trezzolani, Marco Manente, Franco Javier Bosi, A. Lucca Fabris, A. Selmo, Melazzi Melazzi Melazzi
Publikováno v: Proceedings of the AIAA Propulsion and Energy Forum and Exposition 2014, 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference (JPC 2014), 28-30 July 2014, Cleveland, Ohio, 1-26
STARTPAGE=1;ENDPAGE=26;TITLE=Proceedings of the AIAA Propulsion and Energy Forum and Exposition 2014, 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference (JPC 2014), 28-30 July 2014, Cleveland, Ohio
In this communication we report on a combined experimental-numerical activity thas was conducted to assess the antenna-plasma interaction within a Helicon plasma source for space thrusters. The experiment is based on a versatile, re-configurable set-
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::6fb0fb15e21cbc7dc3af24c05e2a3713
https://doi.org/10.2514/6.2014-3407
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8
Design of a thrust balance for RF plasma thruster characterization
Autor: Franco Javier Bosi, Davide Melazzi, A. Selmo, Daniele Pavarin, I. Pita Romero, Fabio Trezzolani, Marco Manente
Publikováno v: 2014 IEEE Metrology for Aerospace (MetroAeroSpace).
In this work we illustrate the design of a thrust balance, to be employed for the experimental characterization of low power helicon plasma thrusters developed at the Center for Aerospace Studies and Activities (CISAS) “G. Colombo” of the Univers
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::6707ee89d8c5f7419e6777a2c07eb732
https://doi.org/10.1109/metroaerospace.2014.6865969
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9
Plasma source optimization for multispecies helicon plasma thruster
Autor: Daniele Pavarin, Davide Melazzi, Vito Lancellotti, Franco Javier Bosi, Marco Manente, Fabio Trezzolani
Publikováno v: Proceedings of the AIAA Propulsion and Energy Forum and Exposition 2014, 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference (JPC 2014), 28-30 July 2014, Cleveland, Ohio, 1-6
STARTPAGE=1;ENDPAGE=6;TITLE=Proceedings of the AIAA Propulsion and Energy Forum and Exposition 2014, 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference (JPC 2014), 28-30 July 2014, Cleveland, Ohio
Radiofrequency (RF) magnetized Helicon plasma sources have been proposed for the development of space thrusters, whose thrust efficiency and specific impulse depend on the power coupled into the plasma by the RF antenna that drives the discharge. In
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::d7f60040cd1ae28fba1f491b41ab7325
https://research.tue.nl/nl/publications/77b8dfee-f616-4d50-b246-0531347ba612
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10
Gliding arc plasma assisted N2O dissociation for monopropellant propulsion
Autor: Danil Dobrynin, Franco Javier Bosi
Publikováno v: Journal of Physics D: Applied Physics. 50:025202
In this paper we address the capability of gliding arc (GA) discharges to promote plasma assisted combustion of nitrous oxide gas (N2O) for spacecraft monopropellant thruster applications. N2O is a 'green' propellant with interesting properties, but
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::7d77ee2655cc45764e2fc6fe85dbcb4e
https://doi.org/10.1088/1361-6463/50/2/025202
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