This work focuses on a numerical suite targeted at cathodeless plasma thrusters. A Global Model is used for a preliminarily estimate of the propulsive performance. The code 3D-VIRTUS solves self-consistently the plasma transport with a fluid approach and the electromagnetic wave propagation in the plasma source. Starfish and SPIS are used to handle the magnetic nozzle region via a fully kinetic Particle-in-Cell approach. Starfish solves the plasma dynamics in a 2D axisymmetric domain and has been coupled to 3D-VIRTUS in order to estimate the propulsive performance. SPIS is a 3D PIC code used mainly to study the interactions between the satellite and the plume. Results have been benchmarked against thrust measurements performed on a low powe...
This article is devoted to the presentation of a semianalytical model of a helicon plasma thruster b...
Electrical thrusters can be used as a useful alternative to the chemical thrusters, the major domina...
In the recent years the PIC simulations of plasma sources have become increasingly important to inve...
This work focuses on a numerical suite targeted at cathodeless plasma thrusters. A Global Model is u...
A Helicon Plasma Thruster is an electric propulsion system in which the thrust is attained accelerat...
Recent advances in plasma-based propulsion systems have led to the development of electromagnetic Ra...
The future of space explorations will not register a big evolution until new families of engines wil...
Radiofrequency (RF) magnetized Helicon plasma sources have been proposed as propulsive devices for s...
Electric propulsion is gaining popularity in space industry. This type of propulsion is replacing ch...
This thesis is concerned with characterising the plume expansion in the magnetic nozzle of a helicon...
Recent advances in plasma-based propulsion systems have led to the development of electromagnetic (R...
International audienceElectric propulsion can reach higher exhaust velocities compared to chemical s...
This article is devoted to the presentation of a semianalytical model of a helicon plasma thruster b...
Electrical thrusters can be used as a useful alternative to the chemical thrusters, the major domina...
In the recent years the PIC simulations of plasma sources have become increasingly important to inve...
This work focuses on a numerical suite targeted at cathodeless plasma thrusters. A Global Model is u...
A Helicon Plasma Thruster is an electric propulsion system in which the thrust is attained accelerat...
Recent advances in plasma-based propulsion systems have led to the development of electromagnetic Ra...
The future of space explorations will not register a big evolution until new families of engines wil...
Radiofrequency (RF) magnetized Helicon plasma sources have been proposed as propulsive devices for s...
Electric propulsion is gaining popularity in space industry. This type of propulsion is replacing ch...
This thesis is concerned with characterising the plume expansion in the magnetic nozzle of a helicon...
Recent advances in plasma-based propulsion systems have led to the development of electromagnetic (R...
International audienceElectric propulsion can reach higher exhaust velocities compared to chemical s...
This article is devoted to the presentation of a semianalytical model of a helicon plasma thruster b...
Electrical thrusters can be used as a useful alternative to the chemical thrusters, the major domina...
In the recent years the PIC simulations of plasma sources have become increasingly important to inve...