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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

    2016-09-28

    Time

    14:45

    Room

    Zapopan

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

    • Co-Chair: Dr. Vanessa Vial, SAFRAN, France;

    • Rapporteur: Mr. Norbert Puettmann, Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Germany;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    KEYNOTE: Beamed Energy Propulsion for future space launchers

    30'

    confirmed

    Prof. Kimiya Komurasaki

    University of Tokyo

    Japan

    2

    Electrical Propulsion Application in China

    15'

    confirmed

    Mr. Min Wang

    China Academy of Space Technology (CAST)

    China

    3

    ELECTRIC PROPULSION IN GERMANY: STATUS OF THE HEMP SYSTEM DEVELOPMENT, PRELIMINARY RESULTS OF THE LIFETIME TEST

    15'

    confirmed

    Mr. Norbert Püttmann

    DLR, German Aerospace Center

    Germany

    4

    Electric Propulsion activities in Airbus DS 2016

    15'

    confirmed

    Mrs. Nicoletta Wagner

    Airbus DS GmbH

    Germany

    5

    Application of pyrolytic graphite grids for a 20 mN ion thruster

    15'

    confirmed

    Mr. Yoshiki Matsunaga

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    6

    Development of a 10kW prototype ion thruster

    15'

    confirmed

    Mr. yide zhao

    Lanzhou Institute of Physics, China Academy of Space technology

    China

    7

    Micro-propulsion based on vacuum arcs: Accessible technologies for CubeSat missions

    15'

    confirmed

    Mr. Jonathan Kolbeck

    George Washington University

    United States

    8

    PPS®1350-E development status

    15'

    confirmed

    Dr. Vanessa Vial

    Snecma

    France

    9

    effect of magnetic field configuration and anode configuration on 5 kw class anode layer type hall thruster

    15'

    confirmed

    Mr. Yusuke Egawa

    Kyushu University

    Japan

    10

    Experimental research of radio-frequency ion thruster

    15'

    confirmed

    Mr. Ruslan Akhmetzhanov

    Research Institute of Applied Mechanics and Electrodynamics (RIAME), MAI

    Russian Federation

    11

    Resistojet design for solid iodine propellant

    15'

    confirmed

    Mr. Mario Angel Andrade Gonzalez

    Mexico

    12

    Discharge and physical characteristics of an ablative liquid-fed pulsed plasma thruster for small satellites

    15'

    withdrawn

    Dr. William Yeong Liang Ling

    University of Tokyo

    Japan

    13

    DEVELOPMENT OF A HARDWARE-IN-THE-LOOP TEST FACILITY USED FOR CHARACTERIZING THE NEW PULSED PLASMA THRUSTER PETRUS

    15'

    confirmed

    Mr. Christoph Montag

    Institute of Space Systems, Universität Stuttgart

    Germany

    14

    Operating the alternative propellant iodine in radio frequency ion thrusters

    15'

    withdrawn

    Ms. Nina Sarah Mühlich

    Justus-Liebig Universität Giessen

    Germany