RF Helicon-based Inductive Plasma Thruster (IPT) Design for an Atmosphere-Breathing Electric Propulsion system (ABEP)-Reference-Cited by-同舟云学术

RF Helicon-based Inductive Plasma Thruster (IPT) Design for an Atmosphere-Breathing Electric Propulsion system (ABEP)

Published:2020-11 Issue: Volume:176 Page:476-483
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Romano F.^ORCID,Chan Y.-A.,Herdrich G.^ORCID,Traub C.,Fasoulas S.,Roberts P.C.E.^ORCID,Smith K.^ORCID,Edmondson S.,Haigh S.^ORCID,Crisp N.H.^ORCID,Oiko V.T.A.,Worrall S.D.,Livadiotti S.^ORCID,Huyton C.,Sinpetru L.A.^ORCID,Straker A.^ORCID,Becedas J.,Domínguez R.M.,González D.^ORCID,Cañas V.^ORCID,Sulliotti-Linner V.^ORCID,Hanessian V.,Mølgaard A.,Nielsen J.,Bisgaard M.,Garcia-Almiñana D.^ORCID,Rodriguez-Donaire S.^ORCID,Sureda M.^ORCID,Kataria D.,Outlaw R.,Villain R.,Perez J.S.,Conte A.,Belkouchi B.,Schwalber A.,Heißerer B.

Funder

European Union’s Horizon 2020 research and innovation programme

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference55 articles.

1. The benefits of very low earth orbit for earth observation missions;Crisp;Prog. Aerosp. Sci.,2020

2. F. Romano, T. Binder, G. Herdrich, S. Fasoulas, T. Schönherr, Air-Intake design investigation for an air-breathing electric propulsion system, in: 34th International Electric Propulsion Conference, Kobe, Japan, IEPC 2015 269b, 2015.

3. F. Romano, T. Binder, G. Herdrich, T. Schönherr, Intake design for an atmosphere-breathing electric propulsion system, in: Space Propulsion 2016, Roma, Italy, SP2016 3124981, 2016.

4. System analysis and test-bed for an atmosphere-breathing electric propulsion system using an inductive plasma thruster;Romano;Acta Astronaut.,2018

5. F. Romano, G. Herdrich, S. Fasoulas, N.C.S. Edmondson, S. Haigh, R. Lyons, V.A. Oiko, P. Roberts, K. Smith, J. Becedas, G. González, I. Vázquez, A.B. nd K. Antonini, K. Bay, L. Ghizoni, V. Jungnell, J. Morsbøl, T. Binder, A. Boxberger, D. Garcia-Alminana, S. Rodriguez-Donaire, D. Kataria, M. Davidson, R. Outlaw, B. Belkouchi, A. Conte, J.S. Perez, R. Villain, A. Schwalber, B. Heißerer, Performance evaluation of a novel inductive atmosphere-breathing EP system, in: 35th International Electric Propulsion Conference, Atlanta, USA, IEPC2017 184, 2017.

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