session 1

1

The Development of LOX/LH2 Engine in China

15'

confirmed

Mr. Nan Zhang

Beijing Aerospace Propulsion Institute

China

2

Development Status of the Cryogenic Oxygen/Hydrogen YF-77 Engine for Long-March 5

15'

confirmed

Mr. Weibin Wang

China

3

The VINCI upper stage engine: the demonstration of maturity

15'

confirmed

Mr. Patrick Danous

Snecma

France

4

technology demonstration status of le-x engine

15'

confirmed

Mr. Hideo Sunakawa

Japan Aerospace Exploration Agency (JAXA)

Japan

5

Cyclone-4 Launch Vehicle III stage engine. Ground testing results

15'

Mr. Alexandr Prokopchuk

Yuzhnoye State Design Office

Ukraine

6

Expand of Capabilities of Rocket and Space Complexes with High–Molecular Additives to Liquid Propellant Components

15'

confirmed

Dr. Valeriy Gaponov

JSC NPO Energomash

Russian Federation

7

Development and Test of the LOX/Methane Regenerative Cooled Rocket Engine (2nd Report)

15'

confirmed

Mr. Kohei Taya

IHI Corporation

Japan

8

Technological Demonstration Tests of main Engine for Reusable Sounding Rocket

15'

confirmed

Dr. Tomoyuki Hashimoto

Japan Aerospace Exploration Agency (JAXA)

Japan

9

System analysis and applied study in the field of a choice of rocket engines for perspective reusable launchers.

15'

confirmed

Mr. Yuri Gusev

TSNIIMASH

Russian Federation

10

Overview on Liquid Propulsion System Modeling Tools for Quick-Loop, Engineering and Design Studies

15'

confirmed

Mr. Markus Jäger

Astrium Space Transportation

Germany

11

Propulsion Control System Model for Liquid Rocket Engines Using Intelligent Techniques

15'

Mr. elayaperumal ezhilrajan

Indian Space Research Organization (ISRO)

India

12

Performance Analyses for Propulsion System of CE-2 Satellite with the Extra Missions

15'

confirmed

Mr. Liang Junqiang

Beijing Institute of Control Engineering, China Academy of Space Technology (CAST)

China