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  • IAC-17
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  • session 5
  • 5. Propulsion Technology (2)

    Papers

    1. KEYNOTE: The 1200kN-thrust-class LOX/Kerosene Rocket Engine for China New Generation Launch Vehicle

    2. Modelling of Lunar Lander’s Thruster’s Exhaust Plume Impingement in Vacuum

    3. Experimental investigation of self-excited combustion instabilities with injection coupling in a cryogenic rocket combustor

    4. Numerical Analysis of Combustion and Regenerative Cooling in LOX-Methane Rocket Engine

    5. Performance evaluation of water - hot gas ejector system used in liquid rocket engines

    6. Optical Diagnostics for Characterization of Hypergolic Ignition in a Paraffin-Based Hybrid Rocket

    7. Modeling and experimental validation for the passive Thermodynamic Vent System (TVS) of cryogenic propellant tank

    8. Visco-plastic cyclic stress analysis of a semi-cryogenic engine thrust chamber

    9. catalyst development and testing for ADN-fuel blends

    10. the flow characteristics study of floating ring seal of liquid rocket engine

    11. Effects of numerical simulation models on thermal characteristics of combustion gas flow ejected from gas oxygen/kerosene rocket engine

    12. Challenges in Realizing Instrumentation and Remote control systems for Testing Cryogenic Engine and stage

    13. sensitivity analysis of static parameters for the lox/kerosene rocket engine

    14. Periodic atomization of impinging injectors modulated by back pressure fluctuations