session 4

Title

Electric Propulsion

Description

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

Date

2014-10-01

Time

14:45

Room

714B

IPC members
papers

Order

Time

Paper title

Selection result

Mode

Presentation status

Speaker

Affiliation

Country

1

Development and Measurement of a Microwave Microplasma Source for Micropropulsion

accepted

15'

withdrawn

Mr. Roberto Dextre

United States

2

ELECTRIC PROPULSION DEVELOPMENT FOR DFH-4SP SATELLITE PLATFORM

accepted

15'

no-show

Mr. Xianming Wu

China

3

Development and Testing of a CubeSat with Highly Miniaturised FEEP Thrusters on a Thrust Balance with Sub-Nanonewton Resolution

accepted

15'

confirmed

Prof. Martin Tajmar

TU Dresden

Germany

4

Preliminary Mission Capabilities Assessment of a Magnetically Shielded Miniature Hall Thruster

accepted

15'

confirmed

Mr. Ryan Conversano

UCLA

United States

5

Investigation of a micro ion thruster for microsatellites

accepted

15'

confirmed

Mr. Alex Christou

Royal Military College

Canada

6

Influence of propellant properties on the performance of a pulsed plasma thruster

accepted

15'

no-show

Mr. Hua Zhang

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

China

7

Development of a LaB6 Cathode for High-Power Hall Thrusters

accepted

15'

no-show

Ms. Daniela Pedrini

Università di Pisa

Italy

8

plasma diagnostics of the mu10 microwave ion thruster

accepted

15'

confirmed

Dr. Ryudo Tsukizaki

JAXA

Japan

9

Electric Propulsion in Germany: System activities, Status of the HEMP- thruster development, challenges coming up

accepted

15'

no-show

Mr. Norbert Püttmann

DLR, German Aerospace Center

Germany

10

results from the qualification test campaign and first flight of a pulsed plasma thruster for cubesats (pptcup)

accepted

15'

confirmed

Mr. Simone Ciaralli

University of Southampton

United Kingdom

11

electric propulsion onboard alphabus

accepted

15'

confirmed

Dr. Vanessa Vial

Snecma

France

12

Development Status of Alta HT-5k High Power Hall Effect Thruster

accepted

15'

withdrawn

Dr. Tommaso Misuri

Sitael Spa

Italy

Characteristics of plasma properties in a pulsed plasma thruster using different modified propellants

Merged with 24599

Mr. Hua Zhang

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

China

Dispenser Hollow Cathode Design for Low-Power Hall Effect Thrusters

Merged with 25234

withdrawn

Dr. Riccardo Albertoni

Sitael Spa

Italy