Zobrazeno 1 - 10
of 19
pro vyhledávání: '"Tommaso Misuri"'
Autor:
Frank Jansen, Tommaso Andreussi, Giovanni Cesarretti, Manfred Ehresmann, Julia Grill, Georg Herdrich, Ikkoh Funaki, Nathalie Girard, Jan Thimo Grundmann, David Krejci, Hans Leiter, Frederic Masson, Volker Maiwald, Tommaso Misuri, Stephane Oriol, Antonio Piragino, Alexander Reissner, Lars Schanz
Publikováno v:
EPJ Techniques and Instrumentation, Vol 10, Iss 1, Pp 1-17 (2023)
Abstract This review deals with the selection of the electric propulsion system (EPS) for the internationally developed and designed, primary nuclear-electric space tug International Nuclear Power and Propulsion System (INPPS). INPPS is scheduled for
Externí odkaz:
https://doaj.org/article/b2e8067d281e4ca5bbd8aa5b038d94d6
Publikováno v:
Aerospace, Vol 7, Iss 7, p 96 (2020)
SITAEL is active in the field of electric propulsion and is involved in the development of different thruster technologies—mainly Hall thrusters (HTs)—of power levels ranging from 100 W up to 20 kW. Low-power HTs are the most effective choice to
Externí odkaz:
https://doaj.org/article/3767a44b8229489b8f46120027c5d189
Publikováno v:
Aerospace, Vol 7, Iss 96, p 96 (2020)
Aerospace; Volume 7; Issue 7; Pages: 96
Aerospace; Volume 7; Issue 7; Pages: 96
SITAEL is active in the field of electric propulsion and is involved in the development of different thruster technologies—mainly Hall thrusters (HTs)—of power levels ranging from 100 W up to 20 kW. Low-power HTs are the most effective choice to
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::1a428b59765b0ec2fee19f9398c58871
https://www.mdpi.com/2226-4310/7/7/96
https://www.mdpi.com/2226-4310/7/7/96
Publikováno v:
IEEE Transactions on Plasma Science. 46:296-303
Low-power Hall effect thrusters (HETs) belong to a class of electric thrusters with an operating power lower than 500 W. The application of this class of HETs is suited for small satellites for telecommunications and Earth observation missions. Sitae
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3cee65cc81f8a16b08ec32a2e218d507
https://doi.org/10.1109/tps.2017.2778317
https://doi.org/10.1109/tps.2017.2778317
Autor:
Tommaso Misuri, Alexandros Manoudis, Luca Benetti, Lorenzo Fontani, Luca Onida, Spiridon Savvas, Pavlos Ramnalis
Publikováno v:
2019 European Space Power Conference (ESPC).
The Microsatellite Electric Propulsion System (MEPS) program has been originated by the increasing need to provide a low cost and low power Electric Propulsion System (EPS) for small satellites (
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7901d4629194b4c63d88689969c2c74c
https://doi.org/10.1109/espc.2019.8932048
https://doi.org/10.1109/espc.2019.8932048
Publikováno v:
Scopus-Elsevier
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::48b22039e55dc204530e93c3376e5d35
http://hdl.handle.net/11568/1078206
http://hdl.handle.net/11568/1078206
Publikováno v:
Aerospace; Volume 4; Issue 2; Pages: 26
Hollow cathodes are electron sources used for the gas ionization and the beam neutralization in both ion and Hall effect thrusters (HETs). A reduction of power and propellant consumption from the cathode is particularly needed in small satellite appl
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::f9b6e8ba6bf02769e339ed576d96ffa1
Publikováno v:
E3S Web of Conferences
E3S Web of Conferences, Vol 16, p 15002 (2017)
E3S Web of Conferences, Vol 16, p 15002 (2017)
In order to maximize system mass and cost savings, a Hall Effect Thruster Direct Drive Approach shall ideally get away with the need to provide galvanic isolation for the Anode voltage. In this respect, we present some experimental data aiming at cha
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::0c6112daf465bcda67a9881bd59de9d2
Autor:
Pavlos Ramnalis, Silvia d’Argliano, Luca Onida, Tommaso Misuri, Dimitrios Malamas, Davide Caniglia, Spiridon Savvas, Luca Benetti, Lorenzo Fontani, Alexandros Manoudis
Publikováno v:
E3S Web of Conferences, Vol 16, p 15004 (2017)
The Micro Satellite Electric Propulsion System (MEPS) program has been originated by the increasing need to provide a low-cost and low-power Electric Propulsion System (EPS) for small satellites ( 92%), small size and weight and high reliability. Its
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::a70a1ab85949d109f4ffcff14cb67be6
https://doi.org/10.1051/e3sconf/20171615004
https://doi.org/10.1051/e3sconf/20171615004