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

2013-09-27

Time

13:30

Room

208A

IPC members
papers

Order

Time

Paper title

Selection result

Mode

Presentation status

Speaker

Affiliation

Country

1

radio wave and ion cyclotron thruster

accepted

15'

confirmed

Mr. Harshit Bisen

SRM University Chennai

India

2

A NOVEL COMBINED PROPULSION CONCEPT FOR DEEP SPACE MISSIONS

accepted

15'

confirmed

Ms. Ragini Ramachandran

Embry-Riddle Aeronautical University

United States

3

FAST Z-PINCH THRUSTER FOR SPACE TUGS

accepted

15'

confirmed

Mr. Patrick Giddens

UAHuntsville

United States

4

Experimental tests of the Mach Effect Thruster.

accepted

15'

confirmed

Prof. Heidi Fearn

California State University

United States

5

ADVANCED SOLAR THERMAL PROPULSION WITH SPECTRAL-SELECTIVE MULTI-STAGED CONCENTRATOR-ABSORBER SYSTEM

accepted

15'

Prof. Sergey Finogenov

Moscow Aviation Institute

Russian Federation

6

Investigation on Status and Prospective Application of Gelled Propellants

accepted

15'

confirmed

Dr. Shuang Liu

The 41st Institute of the Sixth Academy of Aerospace Science & Industry Corp

China

7

A Study of Laser propulsion: An Overdriven detonation mode for a laser-absorption wave

accepted

15'

withdrawn

Mr. Joseph Ofosu

University of Tokyo

Japan

8

Numerical study on working processes of a novel laser ablation thruster with electromagnetic acceleration

accepted

15'

Mr. Daixian Zhang

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

China

9

LightForce: Refined Laser Propulsion Force Model

accepted

15'

withdrawn

Mr. Fan Yang Yang

National Aeronautics and Space Administration (NASA), Ames Research Center / USRA

United States

10

Experimental Research on Continuous Detonation Engine

accepted

15'

Mr. Tianyi Shi

Peking University Health Science Center

China

11

Effects of Different Types of Diverging Nozzle on Propulsion Performance of Continuous Detonation Engine (CDE)

accepted

15'

Dr. Ugur Guven

United States

12

optimum control of ramjets at high flight Mach number and wide-range working conditions

accepted

15'

confirmed

Ms. Baoe Yang

Xi'an Aerospace Propulsion Institute

China