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Showing 1 to 6 of 6 for “"Plasma Propulsion"”.

  1. Theoretical studies of the VASIMR plasma propulsion concept

    … by the Variable Specific Impulse Magnetoplasma Rocket (VASIMR) project. The VASIMR device has a magnetic mirror configuration and consists of three main components: a low energy helicon plasma source, which creates cold plasma via rf-discharge; an ion cyclotron-resonance heating (ICRH) …

    texas Repository record for Theoretical studies of the VASIMR plasma propulsion concept (opens in a new tab)

  2. Comparative simulations of conceptual ion extractors for use in asymmetric inertial electrostatic confinement

    Many deep space propulsion missions currently use ballistic trajectories to reach their destinations. To reduce the times of flight, electric or plasma based propulsion systems are used. While Hall Effect thrusters are the general standard for plasma propulsion, new technologies can enable shorter …

    uiuc Repository record for Comparative simulations of conceptual ion extractors for use in asymmetric inertial electrostatic confinement (opens in a new tab)

  3. Plasma flow and acceleration in the magnetic mirror and nozzle geometries

    … investigates key physics governing transonic plasma flow within converging-diverging magnetic field (magnetic nozzle) configurations as used in fusion open mirror systems and plasma propulsion applications. In such configurations, plasma is accelerated from subsonic to supersonic velocities …

    sask Repository record for Plasma flow and acceleration in the magnetic mirror and nozzle geometries (opens in a new tab)

  4. Thermal Modelling and Validation of Heat Profiles in an RF Plasma Micro-Thruster

    <p>The need and demand for propulsion devices on nanosatellites has grown over the last decade due to interest in expanding nanosatellite mission abilities, such as attitude control, station-keeping, and collision avoidance. One potential micro-propulsion device suitable for nanosatellites is an …

    calpoly Repository record for Thermal Modelling and Validation of Heat Profiles in an RF Plasma Micro-Thruster (opens in a new tab)

  5. A Computational Framework for Dimensionally Reduced Particle Dynamics in Magnetic Nozzle Fields: An Adiabatic Invariant Approach

    This thesis investigates a dimensional reduction strategy for modeling charged particle trajectories in electromagnetic fields representative of magnetic nozzle expansion regions. By employing Julia’s DifferentialEquations.jl and Python’s scientific libraries, particle trajectories are integrated …

    sask Repository record for A Computational Framework for Dimensionally Reduced Particle Dynamics in Magnetic Nozzle Fields: An Adiabatic Invariant Approach (opens in a new tab)