session 3

Title

Propulsion Technology (1)

Description

This session included all science and technologies supporting all aspects of space propulsion. The emphasis in this session is plased in particular components for propulsion.

Date

2014-10-01

Time

09:45

Room

714B

IPC members
papers

Order

Time

Paper title

Selection result

Mode

Presentation status

Speaker

Affiliation

Country

1

An overview of experimental activities and results addressing the development of LOX/LCH4 rocket engine technology in the Italian HYPROB program

accepted

15'

confirmed

Dr. Vito Salvatore

CIRA Italian Aerospace Research Center, Capua

Italy

2

Status and Future Perspectives of the CMC Rocket Thrust Chamber Development at DLR

accepted

15'

confirmed

Mr. Markus Ortelt

Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR)

Germany

3

European Cold Gas Micro Propulsion System reached TRL-9 on board GAIA S/C. Discussion on in flight performance and system flexibly and capabilities, for being implemented in other missions requiring ultra-fine satellite positioning and att

accepted

15'

confirmed

Mr. Aldo Polli

Selex ES S.p.A

Italy

4

Aerojet Rocketdyne Propulsion for Next Generation GEO ComSat Platforms

accepted

15'

confirmed

Ms. Olwen Morgan

Aerojet Rocketdyne

United States

5

Feasibility Analysis and Testing Results of Cold Gas Propulsion System

accepted

15'

confirmed

Mr. Surmit Bhui

University of Petroleum and Energy Studies

India

6

Investigations on the effect of variations in characteristic length(L*) and contraction ratio of the combustion chamber on the performance of a liquid hypergolic bipropellant thruster

accepted

15'

confirmed

Dr. NARAYANAN V

Liquid Propulsion System centre

India

7

Propulsion demonstrators in ESA FLPP 3 serving the competitiveness of European launchers

accepted

15'

confirmed

Mr. Jean-Noel CARUANA

European Space Agency (ESA)

France

8

Developing and testing new composite catalytic bed for decomposition of 98% HTP

accepted

15'

confirmed

Dr. Grzegorz Rarata

Warsaw Institute of Aviation

Poland

9

A scheme study for minimizing weight of pressurization system on KSLV-II upper stage

accepted

15'

confirmed

Mr. Youngsuk Jung

Korea Aerospace Research Institute (KARI)

Korea, Republic of

10

An Experimental Study of LOX/Methane Subscale Injector

accepted

15'

confirmed

Mr. Yuan Tian

Beijing Aerospace Propulsion Institute

China

12

apogee hydrogen peroxide-ethanol rocket propulsion. ecological compatibility, safety and new power opportunities

accepted

15'

confirmed

Mr. Yulian Protsan

The Laboratory of Advanced Jet Propulsion

Ukraine

14

Experimental and numerical study of flame structure and combustion dynamics in a shear coaxial injector with GH2/GO2

accepted

15'

confirmed

Dr. Yue HAN

China Eastern Airlines Corporation Limited

China