session 1

1

LOx/Methane Re-usable Propulsion System Development with implementation of Concurrent Engineering

15'

confirmed

Mr. Paul Valton

Airbus Defence and Space - Space Systems

France

2

NASA Space Launch System Advanced Booster Risk Reduction Status Report

15'

confirmed

Mr. Steve Cook

Dynetics

United States

3

Technology Demonstration Results of LE-X Engine

15'

withdrawn

Mr. Shusuke Hori

Japan Aerospace Exploration Agency (JAXA)

Japan

4

numerical simulation of a lo2-ch4 rocket engine demonstrator

15'

confirmed

Mr. Daniele Cardillo

CIRA Italian Aerospace Research Center, Capua

Italy

5

Development status of a 200 kN thrust Cryogenic upper stage engine for ISRO’s next generation launch vehicle

15'

confirmed

Dr. Vanniyaperumal Narayanan

Indian Space Research Organization (ISRO)

India

6

Flight testing of Indian Cryogenic Upper Stage

15'

confirmed

Dr. Vanniyaperumal Narayanan

Indian Space Research Organization (ISRO)

India

7

The Future of Cryogenic Propulsion

15'

confirmed

Mr. Christophe Bonhomme

Centre National d'Etudes Spatiales (CNES)

France

8

Modernization of powerful LOX-kerosene LPRE of NPO Energomash by change of fuel «kerosene» on «methane»

15'

confirmed

Mr. Vladimir Sudakov

JSC NPO Energomash

Russian Federation

9

modeling study on natural circulation precooling for cryogenic liquid rocket propulsion system

15'

withdrawn

Mr. Shiqiang Chen

China Academy of Launch Vehicle Technology, China

China

10

Design and Demonstration Tests of LOX/LH2 Engine for Reusable Sounding Rocket

15'

confirmed

Mr. Yuya FUKUDA

Mitsubishi Heavy Industries Ltd. Japan

Japan

11

student design/build/test of a throttleable lox-lch4 thrust chamber

15'

confirmed

Mr. Michael Bedard

Purdue University

United States

12

The VINCI propulsion system : new steps toward qualification

15'

confirmed

Mr. Patrick Danous

Snecma

France