rootbrowseIAC-15C4session 11. Propulsion System (1)Papers1. The Development Plan of the First and the Second Stage Engines for the Japanese Next Flagship Launch System2. Creation of family of LPRE for advanced Russian and foreign launch-vehicles on the basis of RD191 engine3. Advancement and Future Application of Space Propulsion Technology Using Hydrocarbon Propellants in China4. The Future of Liquid Propulsion: the French view5. Results of LE-X engine technology demonstration6. VINCI®, the European reference for Ariane 6 upper stage cryogenic engine7. Development of a LM10-MIRA LOX – LNG expander cycle Demonstrator engine8. firing tests for advanced features and long-life durability of the main engine of the reusable sounding rocket9. Applying a Mature Green Propulsion Solution to Enhance Future Mission Capabilities10. A Novel Green Gel Propellant Based Propulsion System11. Research on thermal decomposition of hydrogen peroxide.12. Dynamic characteristics of open-type swirl injector with pulsating manifold pressure13. a review of china's lox/kerosene stage combustion cycle rocket engine14. Features of the propellant tanks pressurization systems development of the LV upper stages