rootbrowseIAC-18C4session 33. Propulsion Technology (1)Papers2. Carbon-carbon Nozzle Extension Assembly for the RL10 Engines3. additive manufacturing development for le-9 engine4. Influences of structural parameters on atomization and combustion performances of LOX/methane pintle injector5. Development Status of Hydroxylammonium-Nitrate-Based Propulsion System with Discharge Plasma System6. Hybrid Rockets with Nozzles in Ultra-High-Temperature Ceramic Composites7. Comparison of simulation and experimental results for functional verification of a propellant mass-flow regulation device8. Development and Qualification of Turbines for the Vinci Upper Stage Engine for Ariane 69. Status of the Turbopump Development in the LUMEN Project10. systems advantages of electric pump fed upper stage hybrid rocket11. Electrical Pressurization Concept for the Orion-ESM Propulsion System12. Development Status of 500 N - class HTP/TMPDA Bi-propellant Rocket Engine13. Development of 10N Mark-2 Thruster for Spacecraft Applications14. Investigation of New Ignition Systems for Future Launcher Application15. Modal Propellant Gauging: High-resolution and non-invasive gauging of both settled and unsettled liquids in reduced gravity.