rootbrowseIAC-17C4session 55. Propulsion Technology (2)Papers1. KEYNOTE: The 1200kN-thrust-class LOX/Kerosene Rocket Engine for China New Generation Launch Vehicle2. Modelling of Lunar Lander’s Thruster’s Exhaust Plume Impingement in Vacuum3. Experimental investigation of self-excited combustion instabilities with injection coupling in a cryogenic rocket combustor4. Numerical Analysis of Combustion and Regenerative Cooling in LOX-Methane Rocket Engine5. Performance evaluation of water - hot gas ejector system used in liquid rocket engines6. Optical Diagnostics for Characterization of Hypergolic Ignition in a Paraffin-Based Hybrid Rocket7. Modeling and experimental validation for the passive Thermodynamic Vent System (TVS) of cryogenic propellant tank8. Visco-plastic cyclic stress analysis of a semi-cryogenic engine thrust chamber9. catalyst development and testing for ADN-fuel blends10. the flow characteristics study of floating ring seal of liquid rocket engine11. Effects of numerical simulation models on thermal characteristics of combustion gas flow ejected from gas oxygen/kerosene rocket engine12. Challenges in Realizing Instrumentation and Remote control systems for Testing Cryogenic Engine and stage13. sensitivity analysis of static parameters for the lox/kerosene rocket engine14. Periodic atomization of impinging injectors modulated by back pressure fluctuations