JAUME NAVARRO CAVALLE

Universidad Politécnica de Madrid

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Articles (19)

Collaborators (3)

EDUARDO AHEDO

Universidad Carlos III de Madrid

Mario Merino

Associate professor

Universidad Carlos III de Madrid Escuela Politécnica Superior

FILIPPO CICHOCKI

Universidad Carlos III de Madrid

JAUME NAVARRO CAVALLE

Research Interests

Explore related searches

Contact this professor

Articles (19)

Collaborators (3)

EDUARDO AHEDO

Mario Merino

FILIPPO CICHOCKI

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JAUME NAVARRO CAVALLE

Research Interests

Explore related searches

Contact this professor

Articles (19)

Reconstruction of the transient plume cross-section of a pulsed plasma thruster

Low-frequency oscillations in the magnetic nozzle of a Helicon plasma thruster

Far-field plume characterization of a low-power cylindrical Hall thruster

Pulsed plasma thruster exhaust reconstruction

Thrust measurements of a waveguide electron cyclotron resonance thruster

Emission and performance characterization of ionic liquids for an externally wetted electrospray thruster

Emission and performance characterization of ionic liquids for an externally wetted electrospray thruster

Pulsed plasma thruster exhaust reconstruction

Plume characterization of a waveguide ECR thruster

Impact of propellant temperature on the emission regime of an externally wetted electrospray system using time-of-flight mass spectrometry

Performance characterization of the μ10 electron-cyclotron-resonance ion thruster using alternative propellants: krypton vs. xenon

Ion dynamics in the magnetic nozzle of a waveguide ECR thruster via laser-induced fluorescence spectroscopy

Ion dynamics in the magnetic nozzle of a waveguide ECR thruster via laser-induced fluorescence spectroscopy

Impact of propellant temperature on the emission regime of an externally wetted electrospray system using time-of-flight mass spectrometry

Laser-induced fluorescence spectroscopy on xenon atoms and ions in the magnetic nozzle of a helicon plasma thruster

Laser-induced fluorescence spectroscopy on xenon atoms and ions in the magnetic nozzle of a helicon plasma thruster

Magnetic Nozzle and RPA Simulations vs. Experiments for a Helicon Plasma Thruster Plume

Corrigendum: Macroscopic and parametric study of a kinetic plasma expansion in a paraxial magnetic nozzle (2020 Plasma Sources Sci. Technol. 29 045017)

Mechanically Amplified Milli-Newton Thrust Balance for Direct Thrust Measurements of Electric Thrusters for Space Propulsion

Collaborators (3)

EDUARDO AHEDO

Mario Merino

FILIPPO CICHOCKI

How do I reach out?

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