Coupled global and PIC modelling of the REGULUS cathode-less plasma thrusters operating on xenon, iodine and krypton

Author:

Andrews ShaunORCID,Andriulli RaoulORCID,Souhair NabilORCID,Di Fede Simone,Pavarin Daniele,Ponti FabrizioORCID,Magarotto MirkoORCID

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference55 articles.

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2. J. Muñoz Tejeda, A. Schwertheim, A. Knoll, Water as an Environmentally Friendly Propellant for a Multi-functional Spacecraft Architecture, in: 8th Space Propulsion Conference, no. SP2022 0272, Estoril, Portugal, 2022.

3. K. Holste, W. Gärtner, P. Köhler, P. Dietz, J. Konrad, S. Schippers, P. Klar, A. Müller, P. Schreiner, Search of Alternative Propellants for Ion Thrusters, in: 34th International Electric Propulsion Conference, no. 2015–320, Kobe, Japan, 2015.

4. V. Giannetti, T. Andreussi, A. Leporini, S. Gregucci, A. Rossodivita, M. Andrenucci, D. Estublier, C. Edwards, M.M. Saravia, Electric Propulsion Sytem Trade-Off Analysis Based On Alternative Propellant Selection, in: 5th Space Propulsion Conference, no. SP2016 3125194, Rome, Italy, 2016.

5. Direct experimental comparison of krypton and xenon discharge properties in the magnetic nozzle of a helicon plasma source;Vinci;Phys. Plasmas,2021

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