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Showing 1 to 5 of 5 for “"Helicon Injected Inertial Plasma Electrostatic Rocket (HIIPER)"”.

  1. Analysis of power balance in a helicon plasma source

    This thesis analyses the Helicon Injected Inertial Plasma Electrostatic Rocket (HIIPER), a space propulsion concept consisting of a helicon source for plasma generation and an ion extraction method using a nested pair of inertial electrostatic confinement (IEC) grids that are asymmetrically …

    uiuc Repository record for Analysis of power balance in a helicon plasma source (opens in a new tab)

  2. Investigation of a space propulsion concept using inertial electrostatic confinement

    This thesis discusses the Helicon Injected Inertial Plasma Electrostatic Rocket (HIIPER), a space propulsion concept consisting of a helicon source for plasma generation and an ion extraction method using a nested pair of inertial electrostatic confinement (IEC) grids that are asymmetrically …

    uiuc Repository record for Investigation of a space propulsion concept using inertial electrostatic confinement (opens in a new tab)

  3. Computational and experimental analysis of HIIPER MPD propulsion system

    Helicon Injected Inertial Plasma Electrostatic Rocket (HIIPER) is a deep space electric propulsion system developed on the principles of inertial electrostatic confinement (IEC) fusion and helicon plasma injection. It is a stepping stone towards a variable impulse pulsed fusion rocket. HIIPER

    uiuc Repository record for Computational and experimental analysis of HIIPER MPD propulsion system (opens in a new tab)

  4. Experimental and numerical validation of ion extractor grids

    "The experimental plasma thruster named the Helicon Injected Inertial Plasma Electrostatic Rocket (HIIPER) at the University of Illinois at Urbana-Champaign (UIUC) is currently being investigated. HIIPER features an Inertial Electrostatic Con nement (IEC) grid that is made asymmetrical by cutting …

    uiuc Repository record for Experimental and numerical validation of ion extractor grids (opens in a new tab)

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

    … 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 travel times. The Helicon Injected Inertial Plasma Electrostatic Rocket (HIIPER) is an attempt …

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