session 1

1

Cryogenic flames submitted to high frequency acoustic waves

15'

Mr. Yoann MERY

France

3

Fuel-Rich Gas Generator Development for a LOx/kerosene Space Rocket Engine

15'

Dr. Seonghyeon Seo

Korea Aerospace Research Institute (KARI)

Korea, Republic of

4

Research on the start system of liquid rocket engine

15'

Mr. Chen Wei

China

5

fuel efficient concept for high altitude flight

15'

Mr. VENKATA SANDEEP KATREVULA

India

6

LISA Pathfinder Field Emission Thruster System Development Program

15'

Mr. Davide Nicolini

European Space Agency (ESA)

The Netherlands

7

Investigation of characteristics of the Vega LV fourth stage main engine assembly: low-frequency oscillations stability, lateral disturbances at startup

15'

Dr. Vladimir Shnyakin

Yuzhnoye State Design Office

Ukraine

8

Study on the startup cyclogram of a liquid rocket engine

15'

Mr. Soon-Young Park

Korea Aerospace Research Institute (KARI)

Korea, Republic of

9

Research on launch vehicle servo system based on energy regulating strategy

15'

Dr. Haikuo Shen

China

10

Determination method of optimum main design parameters of LOx-LH2 expander-cycle LRE for reusable OTV(orbital transfer vehicle)

15'

Dr. Igor Nikolaevich Borovik

Moscow Aviation Institute (National Research University, MAI)

Russian Federation

11

advance in system engineering for the development of the vinci engine

15'

Mr. Philippe Caisso

Safran Aircraft Engines

France