rootbrowseIAC-12C4session 11. Propulsion System (1)Papers1. SYMPOSIUM KEYNOTE: The HYPROB Program: Mastering Key Technologies, Design and Testing Capabilities for Space Transportation Rocket Propulsion Evolution2. DEVELOPMENT OF NEW TECHNOLOGIES APPLIED TO LOX-CH4 PROPULSION3. Demonstration of a 600kN class LOX/Methane Rocket Engine4. Injector Conceptions for Usage of LOX/methane Propellant Composition in Liquid-Liquid, Expander and Staged Combustion Cycles of a Liquid Rocket Engine5. OVERVIEW of LNG PROPULSION SYSTEM DEVELOPMENT6. Main Directions of the Pneudraulic Systems Progress of Contemporary Launch Vehicles7. THE DEVELOPMENT AND QUALIFICATION TESTING OF THE SECOND GENERATION HIGH PERFORMANCE 490N LIQUID APOGEE ENGINE8. Reusable Sounding Rocket Engine Design and Manufacturing Status of Development Engine and Components9. Progress of the development of an all-electric control system of a rocket engine10. JSC "NPO Energomash named after academician V.Glushko" - Leading Russian enterprise on the development and production of liquid propellant rocket engines. Experience and prospect.11. Preliminary Design Study of Staged Combustion Cycle Rocket Engine for SpaceLiner High-Speed Passenger Transportation Concept12. Study on combustion characteristics according to recess length for a rocket engine using gas methane/lox as propellants13. Design Optimization of Liquid Rocket Engine using a Genetic Algorithm14. Research on the cooling method for an oxygen rich preburner15. Development and test of the lox/lng regenerative cooled rocket engine