rootbrowseIAC-16C4session 33. Propulsion Technology (1)Papers1. New Achievements in the HYPROB-BREAD LOX/LCH4 Demonstrator Development2. LOX/Methane Thrust Chamber Demonstrator- from Subscale to Full scale Testing3. Spray and Combustion Characteristics of LOX/GH2 Coaxial Injectors at Supercritical Pressures4. ETID Sandwich Nozzle Demonstrator for Upper Stage Engines5. Additive Manufacturing and its applicability on rockets engines6. Fluidic control of transition in dual bell launcher nozzle7. growth of spacecraft propulsion systems in isro8. Development of High Performance Liquid Apogee Motor for Geostationary Spacecraft9. Extending Lifetime of Rocket Engine Combustion Chamber10. Investigation of Dynamics Characteristics of the Hot Gas Bellows of the LOX/Kerosene Rocket Engine11. numerical simulation of combustion stability of coaxial swirl injector12. CFD analysis of Semicryo LOX booster turbopump.13. Numerical Simulation of LRE and HRE Reacting Flowfields14. study of flow characteristics for liquid film in the impinging stream vortex chamber by cfd and experiment