Design of 50 W helicon plasma thruster

D. Pavarin; F. Ferri; M. Manente; D. Curreli; Y. Guclu; Melazzi Davide; D. Rondini; S. Suman; J. Carlsson; C. Bramanti; E. Ahedo; V. Lancellotti; K. Katsonis; G. Markelov

Design of 50 W helicon plasma thruster

D. Pavarin
, F. Ferri
, M. Manente
, D. Curreli
, Y. Guclu
, Melazzi Davide
, D. Rondini
, S. Suman
, J. Carlsson
, C. Bramanti
, E. Ahedo
, V. Lancellotti
, K. Katsonis
, G. Markelov

Electromagnetics

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › Academic › peer-review

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Abstract

This paper is focused on the description of simulation codes developed to design a helicon plasma thruster for a small satellite under development in the research project Helicon plasma hydrazine combined micro (HPH.com) conducted within the 7th Framework Program of the EU by a European consortium.

Original language	English
Title of host publication	Proceedings of the 31st International Electric Propulsion Conference, IEPC-2009, 20-24 September, 2009, Ann Arbor, Michigan
Pages	1-8
Publication status	Published - 2009

Cite this

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title = "Design of 50 W helicon plasma thruster",

abstract = "This paper is focused on the description of simulation codes developed to design a helicon plasma thruster for a small satellite under development in the research project Helicon plasma hydrazine combined micro (HPH.com) conducted within the 7th Framework Program of the EU by a European consortium.",

author = "D. Pavarin and F. Ferri and M. Manente and D. Curreli and Y. Guclu and Melazzi Davide and D. Rondini and S. Suman and J. Carlsson and C. Bramanti and E. Ahedo and V. Lancellotti and K. Katsonis and G. Markelov",

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AU - Pavarin, D.

AU - Ferri, F.

AU - Manente, M.

AU - Curreli, D.

AU - Guclu, Y.

AU - Davide, Melazzi

AU - Rondini, D.

AU - Suman, S.

AU - Carlsson, J.

AU - Bramanti, C.

AU - Ahedo, E.

AU - Lancellotti, V.

AU - Katsonis, K.

AU - Markelov, G.

PY - 2009

Y1 - 2009

N2 - This paper is focused on the description of simulation codes developed to design a helicon plasma thruster for a small satellite under development in the research project Helicon plasma hydrazine combined micro (HPH.com) conducted within the 7th Framework Program of the EU by a European consortium.

AB - This paper is focused on the description of simulation codes developed to design a helicon plasma thruster for a small satellite under development in the research project Helicon plasma hydrazine combined micro (HPH.com) conducted within the 7th Framework Program of the EU by a European consortium.

M3 - Conference contribution

SP - 1

EP - 8

BT - Proceedings of the 31st International Electric Propulsion Conference, IEPC-2009, 20-24 September, 2009, Ann Arbor, Michigan

ER -

Design of 50 W helicon plasma thruster

Abstract

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Cite this