SITAEL HC1 Low-Current Hollow Cathode
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 perform orbit transfer, drag compensation, and de-orbi...
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doaj-3767a44b8229489b8f46120027c5d1892020-11-25T02:36:56ZengMDPI AGAerospace2226-43102020-07-017969610.3390/aerospace7070096SITAEL HC1 Low-Current Hollow CathodeDaniela Pedrini0Cosimo Ducci1Ugo Cesari2Tommaso Misuri3Mariano Andrenucci4Space Propulsion Division, SITAEL, 56121 Pisa, ItalySpace Propulsion Division, SITAEL, 56121 Pisa, ItalySpace Propulsion Division, SITAEL, 56121 Pisa, ItalySpace Propulsion Division, SITAEL, 56121 Pisa, ItalySpace Propulsion Division, SITAEL, 56121 Pisa, ItalySITAEL 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 perform orbit transfer, drag compensation, and de-orbiting maneuvers for small satellites. This paper is dedicated to the activities regarding HC1, the hollow cathode conceived for the 100-W-class Hall thruster under development at SITAEL. Successful test campaigns were performed and are described, with emphasis on the improvements in the cathode design after an extensive research and development phase. The results are presented and discussed, along with future developments of the ongoing activities.https://www.mdpi.com/2226-4310/7/7/96Hall thrusterelectric propulsionhollow cathode |
collection |
DOAJ |
language |
English |
format |
Article |
sources |
DOAJ |
author |
Daniela Pedrini Cosimo Ducci Ugo Cesari Tommaso Misuri Mariano Andrenucci |
spellingShingle |
Daniela Pedrini Cosimo Ducci Ugo Cesari Tommaso Misuri Mariano Andrenucci SITAEL HC1 Low-Current Hollow Cathode Aerospace Hall thruster electric propulsion hollow cathode |
author_facet |
Daniela Pedrini Cosimo Ducci Ugo Cesari Tommaso Misuri Mariano Andrenucci |
author_sort |
Daniela Pedrini |
title |
SITAEL HC1 Low-Current Hollow Cathode |
title_short |
SITAEL HC1 Low-Current Hollow Cathode |
title_full |
SITAEL HC1 Low-Current Hollow Cathode |
title_fullStr |
SITAEL HC1 Low-Current Hollow Cathode |
title_full_unstemmed |
SITAEL HC1 Low-Current Hollow Cathode |
title_sort |
sitael hc1 low-current hollow cathode |
publisher |
MDPI AG |
series |
Aerospace |
issn |
2226-4310 |
publishDate |
2020-07-01 |
description |
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 perform orbit transfer, drag compensation, and de-orbiting maneuvers for small satellites. This paper is dedicated to the activities regarding HC1, the hollow cathode conceived for the 100-W-class Hall thruster under development at SITAEL. Successful test campaigns were performed and are described, with emphasis on the improvements in the cathode design after an extensive research and development phase. The results are presented and discussed, along with future developments of the ongoing activities. |
topic |
Hall thruster electric propulsion hollow cathode |
url |
https://www.mdpi.com/2226-4310/7/7/96 |
work_keys_str_mv |
AT danielapedrini sitaelhc1lowcurrenthollowcathode AT cosimoducci sitaelhc1lowcurrenthollowcathode AT ugocesari sitaelhc1lowcurrenthollowcathode AT tommasomisuri sitaelhc1lowcurrenthollowcathode AT marianoandrenucci sitaelhc1lowcurrenthollowcathode |
_version_ |
1724797911587356672 |