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  • session 1
  • 1. Liquid Propulsion (1)

    Papers

    1. Data-driven emulation models for Rocket Engines injector design

    2. Design of a conical anti-slosh baffle and its experimental validation for slosh stability for the Indian interplanetary mission

    4. Preliminary Test of Hydrogen Peroxide Thermal Decomposition Monopropellant Thruster

    6. Development of an additively manufactured Hydrogen Peroxide / Kerosene 6 kN aerospike breadboard engine

    8. Liquid Upper Stage Demonstrator Engine (LUMEN): Overview and Project Progress

    11. comparison between a 400n electric pump fed hydrogen peroxide/ethanol thruster and the mmh/nto legacy systems

    1003. The results of ground development tests of the RD861K high-altitude liquid-propellant restartable rocket engine

    1005. Ariane 6 Upper Liquid Propulsive Module Qualification

    1007. Experimental characterization and analysis of passive flow separation control of upper stage rocket nozzle during sea-level testing

    1009. Tests to study the influence of the low temperature of structure and propellants on the performance of VEGA Stage 4 main engine

    1012. Experimental & Numerical Investigation of GOX/GCH4 Combustion in 7- Element Sub-scale Combustor