session 4

Title

Electric Propulsion

Description

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

Date

2013-09-25

Time

14:45

Room

208A

IPC members
papers

Order

Time

Paper title

Selection result

Mode

Presentation status

Speaker

Affiliation

Country

1

In-Flight experiments and Development of electric propulsion system on satellite SJ-9A

accepted

12'

confirmed

Prof. Wei Yanming

Beijing Institute of Control Engineering, China Academy of Space Technology (CAST)

China

2

TAL Thruster Development for the Japanese High-Power In-Space Propulsion Project RAIJIN

accepted

12'

confirmed

Dr. Tony Schönherr

University of Tokyo

Japan

3

magneto-plasma rocket propulsion

accepted

15'

withdrawn

Mr. Judin Narlely

SRM University, kattankulathur,chennai

India

4

The Alta FT-150 FEEP microthruster: test results of the pre-qualification campaign

accepted

12'

confirmed

Dr. Angela Rossodivita

Sitael Spa

Italy

5

Ionic Liquid FEEP Thruster Ion Beam Characterization

accepted

15'

Prof. Salvo Marcuccio

Sitael Spa

Italy

6

study on discharge characteristics and mode transition phenomenon in a helicon plasma thruster

accepted

12'

confirmed

Mr. Cheng Yuguo

National University of Defense Technology of the Chinese People's Liberation Army

China

7

Modeling of LaB6 Hollow Cathode Performance and Lifetime

accepted

15'

confirmed

Ms. Daniela Pedrini

Università di Pisa

Italy

8

Design and Development of an Engineering-model Low-power Liquified-gas Resistojet

accepted

12'

Mr. Abdolrahim Rezaeiha

Sharif University of Technology

Iran

9

Status of the HEMP- thruster development for satellite missions

accepted

15'

Mr. Norbert Püttmann

DLR, German Aerospace Center

Germany

10

THE LIPS-200 ION ELECTRIC PROPULSION SYSTEM DEVELOPMENT FOR THE DFH-3B SATELLITE PLATFORM

accepted

12'

confirmed

Prof.Dr. zhang tianping

Lanzhou Institute of Physics

China

11

Numerical Simulation of a System of Formation of an Intense Ion Beam from Gas Discharge Plasma of an Ion Thruster

accepted

12'

confirmed

Mr. Ruslan Akhmetzhanov

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

Russian Federation

12

Magnetic Nozzle optimization for Plasma Space Propulsion

accepted

12'

withdrawn

Mr. Mario Merino

Universidad Politécnica de Madrid

Spain

13

Feasibility Study of Air-Breathing Pulsed Plasma Thruster

accepted

15'

confirmed

Dr. Tony Schönherr

University of Tokyo

Japan

14

Study on a Double Pulse Discharge Solid Pulsed Plasma Thruster

accepted

12'

confirmed

Mr. Huang Tiankun

Beijing Institute of Technology

China

15

Ethylammonium nitrate is a singular propellant in electrospray propulsion

accepted

12'

withdrawn

Mr. Jan Kolmas

United States