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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

    2012-10-03

    Time

    15:15

    Room

    TS14 (Sala Capri, Palacongressi)

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

    • Chairman: Prof. Mariano Andrenucci, Independent consultant, Italy;

    • 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

    Recent Developments in High Power Electric Propulsion: Outcomes of HiPER Project Activities

    15'

    confirmed

    Dr. Tommaso Misuri

    Sitael Spa

    Italy

    2

    Advancement of a 30 kW solar electric propulsion system capability for nasa human and robotic exploration missions

    15'

    confirmed

    Mr. Bryan K. Smith

    NASA Glenn Research Center

    United States

    3

    APPLICATION OF STATIONARY PLASMA THRUSTERS FOR SPACECRAFT INSERTION INTO THE GEOSTATIONARY ORBIT

    15'

    confirmed

    Dr. Viacheslav Petukhov

    RIAME

    Russian Federation

    4

    Electric propulsion subsystem on SGEO satellite: architecture, functional features and future enhancements

    15'

    withdrawn

    Mr. Marco De Tata

    OHB System AG-Bremen

    Germany

    5

    Magnetic field tuning during the testing of Stationary Plasma Thruster

    15'

    confirmed

    Mr. Krishna Mohan Shanbhogue

    Indian Space Research Organization (ISRO)

    India

    6

    High-Power Hall Propulsion System Development at NASA Glenn Research Center

    15'

    confirmed

    Dr. George Schmidt

    National Aeronautics and Space Administration (NASA)

    United States

    7

    The Alta FT-150 Thruster for the LISA Pathfinder and LISA/NGO Missions

    15'

    confirmed

    Mr. Luca Paita

    Sitael Spa

    Italy

    8

    Development, integration and test of Power Electronic equipments for controlling Thrusters in the Micro-Newton range

    15'

    confirmed

    Mr. Luca Ceruti

    Galileo Avionica S.p.A.

    Italy

    9

    Electric propulsion verification - Managing measurement uncertainty

    15'

    confirmed

    Mr. Richard Blott

    Space Enterprise Partnerships Limited

    United Kingdom

    10

    Design of Air Intake for Air Breathing Ion Engine

    15'

    confirmed

    Mr. Yasuyoshi Hisamoto

    The Graduate University of Advanced Studies

    Japan

    11

    Performance improvement of a carbon nanotube field emission cathode

    15'

    confirmed

    Dr. Yasushi Ohkawa

    JAXA

    Japan

    12

    Analysis of VASIMR Air-Breathing Thruster

    15'

    confirmed

    Mr. Charles Moser

    Cranfield University

    United Kingdom

    13

    Electroplating techniques for improving electrochemical resistance of silicon and nickel MEMS electrospray thrusters

    Poster

    confirmed

    Ms. Natalya Brikner

    Massachusetts Institute of Technology (MIT)

    United States

    14

    Insight into endurance enhancement of ecr microwave discharge neutralizer

    Poster

    confirmed

    Mr. Wataru Ohmichi

    Tokyo University, Graduate school

    Japan

    15

    A Plug and Play Pulsed Electrothermal Thruster for CubeSat Applications

    Poster

    confirmed

    Mr. Matthias Lau

    University of Stuttgart

    Germany

    16

    Comparative study on numerical simulation by kinetic and fluid models for mhd accelerator

    Poster

    confirmed

    Mr. Ulderico Spadavecchia

    Nagaoka University of Technology

    Japan

    17

    Effects of discharge characteristics on propellant ablation in Pulsed Plasma Thruster

    Poster

    Dr. Rui Zhang

    College of Aerospace and Materials Engineering, National University of Defense Technology

    China

    18

    The effect of discharge loop inductance compensation on hall thruster

    Poster

    confirmed

    Ms. zhang wen

    China Academy of Launch Vehicle Technology (CALT)

    China

    19

    Non conventional electrod configuration in electrogasdinamics tests.

    Poster

    confirmed

    Mr. Enrique Calcagni

    Instituto Universitario Aeronautico

    Argentina

    20

    A New Design of Power Processing Unit for Hall Thrusters

    Poster

    withdrawn

    21

    Advanced plasma propulsion with magnetic nozzles

    Poster

    confirmed

    Mr. Mario Merino

    Universidad Politécnica de Madrid

    Spain

    22

    FEEP characterization in terms of mass efficiency and specific impulse versus emitter geometry

    Poster

    Mr. Luca Paita

    Sitael Spa

    Italy

    23

    FEEP Thruster Characterization in Function of Emitter Hydraulic Resistance

    Poster

    Mr. Luca Paita

    Sitael Spa

    Italy

    24

    Particle In Cell simulation of FEEP Thruster Plume

    Poster

    Mr. Luca Paita

    Sitael Spa

    Italy

    25

    Surface electrical resistivity of randomly Caesium contaminated FEEP ceramic

    Poster

    Mr. Luca Paita

    Sitael Spa

    Italy

    26

    A new power processing control unit for a 20 mN class ion engine system

    Poster

    confirmed

    Dr. Hiroshi Nagano

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    27

    A 500 MicroNewton Class FEEP Thruster

    Poster

    Mr. Luca Paita

    Sitael Spa

    Italy

    28

    Design and research on pulsed high thrust resistojet

    Poster

    confirmed

    Dr. Lukasz Mezyk

    Warsaw University of Technology (WUT)

    Poland

    Alta FT-150 FEEP: overview and development status

    with 16068

    Mr. Luca Paita

    Sitael Spa

    Italy

    AN EXPERIMENTAL INVESTIGATION OF A 100-KW CLASS APPLIED FIELD MPD THRUSTER

    with 15323

    Dr. Riccardo Albertoni

    Sitael Spa

    Italy

    Characterization of Dispenser Hollow Cathode Emitter for its acceptance in Hollow Cathode Assembly.

    with 15595

    confirmed

    Mr. Karthikeyan Nandakumar

    LPSC, ISRO

    India