session 8

Title

Advanced and Combined Propulsion Systems

Description

The session is for the presentation of advanced propulsion concepts being studied or considered. The advanced concepts should seek to deliver breakthroughs in overcoming the limitations of propulsion systems in current use or development. For advanced concepts technologies should normally be in the range TRL 0 to TRL 2. Advanced concepts with higher TRL technologies may also be presented where a combination of propulsion technologies can lead to performance breakthroughs which can not be achieved with a single technology. A combination can include for example both chemical and electric or solid and liquid chemical.

Date

2014-10-03

Time

13:30

Room

714B

IPC members
papers

Order

Time

Paper title

Selection result

Mode

Presentation status

Speaker

Affiliation

Country

1

Introduction and Performance Analysis of the Solar Wind Ion Focusing Thruster (SWIFT)

accepted

20'

confirmed

Mr. Thomas Gemmer

North Carolina State University

United States

2

orbital maneuver of satellite using solar sail

accepted

20'

no-show

Mr. Logesh Sadasivam

SRM University, kattankulathur,chennai,INDIA

India

3

optimal design of conduction-cooled superconducting magnet for magneto plasma sail

accepted

20'

confirmed

Mr. Yoh Nagasaki

Research Institute for Sustainable Humanosphere, Kyoto University

Japan

4

SOLAR ELECTRO REACTION ENGINE

accepted

20'

no-show

Ms. Safoora Tanbakouei

Space Generation Advisory Council (SGAC)

Iran

5

Second Generation EmDrive Propulsion applied to SSTO Launcher and Interstellar Probe.

accepted

20'

confirmed

Mr. Roger Shawyer

Satellite Propulsion Research Ltd

United Kingdom

6

Creation of LPRE with the use of detonation combustion in the chamber

accepted

15'

withdrawn

Mr. Vladimir Sudakov

JSC NPO Energomash

Russian Federation

7

Numerical Simulation of Combustion Characteristics of Boron Particle in Forced Convective Environment

accepted

20'

no-show

Mr. Chuanbo Fang

National University of Defense Technology

China

8

High Resolution Numerical Simulation on Dynamics of Intake Shock Motion

accepted

20'

confirmed

Ms. Qin Yan-ping

Xi'an Aerospace Propulsion Institute

China