rootbrowseIAC-18C4session 1010. Propulsion Technology (3)Papers1. KEYNOTE: Green Solutions for Space Propulsion2. Combustion Characterstics of Lox-Methane in Swirl Coaxial Injector Hydrogen Propulsion System3. Research on the key technology of the ‘swing behind pump’ thrust vector regulation architecture used in large thrust LOX/kerosene engine4. Maximizing side force generation in aerospike nozzles for attitude and trajectory control5. Cryo-Laboratory for the Investigation of Propellant Behaviour and Development of Propellant Management Technologies6. Numerical investigation on performance of fuel booster turbopump for staged combustion cycle based rocket engine.7. Hydraulic Development Testing of the Pressurization Concept for the Orion-ESM Propulsion System8. FLPP3: TEST RESULTS OF FULL ELECTRICALLY ACTUATED ENGINE VALVES9. Sloshing and Pressurization Tests for Membrane Tank: Tests, Validation and Models10. Test of a highly reusable LOx/Methane gas generator demonstrator in a flight-like configuration11. Identification and Maturation of Technologies for Future Liquid Propellant Engines12. CFD simulation of reactive flow in cryogenic rocket nozzle and performance prediction of LVM III CE20 nozzle13. The pyronumeric, a new technology to answer to the future launchers challenges