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  • session 4

    Title

    Electric Propulsion

    Description

    This session is dedicated to all aspects of electric propulsion technologies, systems and applications.

    Date

    2010-09-29

    Time

    15:15

    Room

    Club A

    IPC members
    • Chairman: Prof. Garri A. Popov, Research Institute of Applied Mechanics and Electrodynamics (RIAME), MAI, Russian Federation;

    • Chairman: Mr. Richard Blott, British Interplanetary Society, United Kingdom;

    • Rapporteur: Mr. Rafael Spears, L-3 Communications, United States;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    development of the ion engine system for slats

    15

    confirmed

    Dr. Hiroshi Nagano

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    2

    A 20kW High Power Hall Effect Thruster for exploration

    15

    confirmed

    Mr. Nicolas Cornu

    Safran Aircraft Engines

    France

    3

    Summary of the 25000 Hour Round-Trip Ion Drive of Hayabusa

    15

    confirmed

    Prof. Kazutaka Nishiyama

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    4

    Design and Testing of a Pulsed Plasma Thruster for Cubesat Application

    15

    withdrawn

    Mr. Francesco Guarducci

    University of Southampton

    United Kingdom

    5

    Development of a Cyrindrical Hall Thruster

    15

    confirmed

    Mr. Shinatora Cho

    The University of TOKYO, Graduate school

    Japan

    6

    Towards very high power electric propulsion

    15

    confirmed

    Mr. Nicolas Cornu

    Safran Aircraft Engines

    France

    7

    Study on Comparative Performance of Advanced Ion Propulsion Engine Systems

    10

    withdrawn

    Mr. JUSTIN CHISM

    United States

    8

    Nanoparticle Accelerator with Lorentz Modulation-NAPALM

    10

    confirmed

    Mr. Istvan Lorincz

    Delft University of Technology (TU Delft)

    The Netherlands

    9

    Influence of Input Energy Increase on Thrust Performance of Coaxial Pulsed Plasma Thruster

    10

    confirmed

    Mr. Yohei Kitazono

    Tokyo Metropolitan University

    Japan

    10

    Influence of structural factors on processes in the low power Hollow Thruster

    10

    Prof. Olexandr Petrenko

    Dniepropetrovsk National University

    Ukraine

    11

    Qualification Test Series of the Indium Needle FEEP Micro-propulsion System for LISA Pathfinder

    10

    confirmed

    Dr. Carsten Scharlemann

    University of Applied Science Wiener Neustadt

    Austria

    12

    A New Power Control Method for Hall Thruster Using Oscillation-Mode-Map

    10

    confirmed

    Dr. Hiroyuki Osuga

    Mitsubishi Electric Corporation

    Japan

    13

    Numerical Simulation of Microwave-Excited Microplasma Thruster with Helium Propellant

    10

    confirmed

    Mr. Takeshi Takahashi

    Kyoto University

    Japan

    14

    an upper atomosphere simulator using ecr discharge for air breathing ion engines

    10

    confirmed

    Mr. Yasuyoshi Hisamoto

    The Graduate University of Advanced Studies

    Japan

    15

    High energy ion production and erosion in hollow cathode microthrusters

    10

    withdrawn

    Dr. Angelo Grubisic

    University of Southampton

    United Kingdom