rootbrowseIAC-21C4session 11. Liquid Propulsion (1)Papers1. Data-driven emulation models for Rocket Engines injector design2. Design of a conical anti-slosh baffle and its experimental validation for slosh stability for the Indian interplanetary mission4. Preliminary Test of Hydrogen Peroxide Thermal Decomposition Monopropellant Thruster6. Development of an additively manufactured Hydrogen Peroxide / Kerosene 6 kN aerospike breadboard engine8. Liquid Upper Stage Demonstrator Engine (LUMEN): Overview and Project Progress11. comparison between a 400n electric pump fed hydrogen peroxide/ethanol thruster and the mmh/nto legacy systems1003. The results of ground development tests of the RD861K high-altitude liquid-propellant restartable rocket engine1005. Ariane 6 Upper Liquid Propulsive Module Qualification1007. Experimental characterization and analysis of passive flow separation control of upper stage rocket nozzle during sea-level testing1009. Tests to study the influence of the low temperature of structure and propellants on the performance of VEGA Stage 4 main engine1012. Experimental & Numerical Investigation of GOX/GCH4 Combustion in 7- Element Sub-scale Combustor