sample of publications
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articles
- Impact of propellant temperature on the emission regime of an externally wetted electrospray system using time-of-flight mass spectrometry. ACTA ASTRONAUTICA. 213:145-155. 2023
- Analysis of a cusped helicon plasma thruster discharge. PLASMA SOURCES SCIENCE & TECHNOLOGY. 32:1-19. 2023
- Performance characterization of the µ10 electron-cyclotron-resonance ion thruster using alternative propellants: krypton vs. xenon. ACTA ASTRONAUTICA. 211:750-754. 2023
- Plume characterization of a waveguide ECR thruster. JOURNAL OF APPLIED PHYSICS. 133:113304-1-113304-14. 2023
- Ion dynamics in the magnetic nozzle of a waveguide ECR thruster via laser-induced fluorescence spectroscopy. JOURNAL OF PHYSICS D-APPLIED PHYSICS. 56:1-10. 2023
- Laser-induced fluorescence spectroscopy on xenon atoms and ions inthe magnetic nozzle of a Helicon plasma thruster. PLASMA SOURCES SCIENCE & TECHNOLOGY. 31:1-12. 2022
- Magnetic Nozzle and RPA Simulatons vs. Experiments for a Helicon Plasma Thruster Plume. Frontiers in Physics. 10:1-15. 2022
- Corrigendum: Macroscopic and parametric study of a kinetic plasma expansion in a paraxial magnetic nozzle (2020 Plasma Sources Sci. Technol.29 045017). PLASMA SOURCES SCIENCE & TECHNOLOGY. 30:1-1. 2021
- Mechanically Amplified Milli-Newton Thrust Balance for Direct Thrust Measurements of Electric Thrusters for Space Propulsion. IEEE TRANSACTIONS ON INSTRUMENTATION AND MEASUREMENT. 70:3505318-1 - 3505318-1. 2020
- Commentary: On helicon thrusters: Will they ever fly?. Frontiers in Physics. 8:1-3. 2020
- Macroscopic and parametric study of a kinetic plasma expansion in a paraxial magnetic nozzle. PLASMA SOURCES SCIENCE & TECHNOLOGY. 29:1-17. 2020
- Experimental characterization of a 1 kW Helicon Plasma Thruster. Vacuum. 149:69-73. 2018
- Electron cooling and finite potential drop in a magnetized plasma expansion. PHYSICS OF PLASMAS. 22:1-11. 2015
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conference contributions
- Experiments and Simulations of a Magnetic Arch Plasma Expansion for Space Propulsion 2023
- 37th International Electric Propulsion Conference Massachusetts Institute of Technology. 1-11. 2022
- Advances on cost-optimized high-pressure flow control unit within Hipatia-project. 1-6. 2022
- Characterization of a low-power Cylindrical Hall Thruster. 1-17. 2022
- Design and preliminary study of a 200W cylindrical hall thruster. 1-11. 2022
- Direct Thrust Measurements of a circular waveguide Electron Cyclotron Resonance Thruster. 1-16. 2022
- Direct Thrust Measurements of the HIPATIA Thruster Unit. 1-10. 2022
- Experimental plume characterization of a low-power Ablative Pulsed Plasma Thruster (APPT). 1-18. 2022
- Preliminary model of the plasma expansion in a magnetic arch thruster (and overview of the first prototype). 1-15. 2022
- Probing xenon atoms and ions velocity in the magnetic nozzle of a helicon plasma thruster. 1-15. 2022
- Results of the first Helicon Plasma Thruster (HPT) coupling test campaign within the HIPATIA project. 1-9. 2022
- Design of an experimental ablative pulsed plasma thruster for micropropulsion. 1-8. 2021
- Hybrid PIC-fluid simulation of a waveguide ECR magnetic nozzle plasma thruster 2021
- The HIPATIA project's initial development stages: setting the basis to bring the Helicon Plasma Thruster and its associated technologies to intermediate-high TRLs. 1-7. 2021
- HIPATIA: a project for the development of the Helicon Plasma Thruster and its associated technologies to intermediate-high TRLs 2020
- An experimental revisit of plasma phenomena on Helicon Plasma Thrusters. 1-8. 2019
- Development and Characterization of the Helicon Plasma Thruster Prototype HPT-03. 1-12. 2019
- Experimental activities at the Electric propulsion and Plasmas Team (EP2- UC3M): an example of an intense testing campaign on the Helicon Plasma Thruster (HPT05M). 1-12. 2019
- Fluid Model of a Hollow Cathode Discharge. 1-24. 2019
- Helicon and ECR plasma sources for space propulsion: Simulation and testing. 788-793. 2019
- Macroscopic Hollow Cathode Modelling: A Variable-Separation Approach. 42-42. 2019
- Mechanically amplified milli-Newton thrust balance for helicon plasma thrusters. 1-17. 2019
- RF Power: Plasma Coupling Experimental Results in a Helicon Plasma Thruster Prototype. 1-8. 2019
- Synergies between space plasma propulsion and magnetic confinement plasma fusion: PROMETEO project. 497-497. 2019
- Trade-off Analysis of C12A7:e-Deposition Techniques Applied to Low Work Function Tethers. 87-87. 2019
- Webcam based in-vacuum tomography of plasma thruster jets. 1-4. 2019
- Work function tuning of graphene oxide by using cesium oxide nanoparticles applied to low work function tethers. 86-86. 2019
- Magnetic nozzles. 1-17. 2018
- Experimental performances of a 1 kW HPT by means of plasma diagnosis 2017
- Optical Emission Spectroscopy diagnostics of heliconplasma thruster operating with Argon. 1-10. 2017
- Electron thermodynamics in the magnetized expansion of a rarefied plume 2016
- Kinetic modelling of collisionless electron cooling on magnetized plasma expansions 2016
- Maiden tests of the HPT05 helicon plasma thruster Prototype 2016
- Analysis of Plasma Impedance in Helicon Antenna Thrusters 2015
- Design and development of a 1kW-class helicon antenna thruster 2015
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Hybrid simulation of a
Magnetic Nozzle plume: exploring magnetized/demagnetized regimes 2015 - Collisionless Electron Cooling in a Magnetic Nozzle 2014
- Design of Helicon Plasma Thruster Subsystems. 3584-3596. 2014
- Investigation of Plasma-wave Interaction in Helicon Antenna Thrusters 2014
- Helicon plasma thrusters: prototypes and advances on modeling 2013
- Space missions potentially benefit or enabled by the prospective use of Helicon Plasma thrusters 2013