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  • session 3
  • 3. Propulsion Technology (1)

    Papers

    1. New Achievements in the HYPROB-BREAD LOX/LCH4 Demonstrator Development

    2. LOX/Methane Thrust Chamber Demonstrator- from Subscale to Full scale Testing

    3. Spray and Combustion Characteristics of LOX/GH2 Coaxial Injectors at Supercritical Pressures

    4. ETID Sandwich Nozzle Demonstrator for Upper Stage Engines

    5. Additive Manufacturing and its applicability on rockets engines

    6. Fluidic control of transition in dual bell launcher nozzle

    7. growth of spacecraft propulsion systems in isro

    8. Development of High Performance Liquid Apogee Motor for Geostationary Spacecraft

    9. Extending Lifetime of Rocket Engine Combustion Chamber

    10. Investigation of Dynamics Characteristics of the Hot Gas Bellows of the LOX/Kerosene Rocket Engine

    11. numerical simulation of combustion stability of coaxial swirl injector

    12. CFD analysis of Semicryo LOX booster turbopump.

    13. Numerical Simulation of LRE and HRE Reacting Flowfields

    14. study of flow characteristics for liquid film in the impinging stream vortex chamber by cfd and experiment