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  • session 3
  • 3. Propulsion Technology (1)

    Papers

    2. Carbon-carbon Nozzle Extension Assembly for the RL10 Engines

    3. additive manufacturing development for le-9 engine

    4. Influences of structural parameters on atomization and combustion performances of LOX/methane pintle injector

    5. Development Status of Hydroxylammonium-Nitrate-Based Propulsion System with Discharge Plasma System

    6. Hybrid Rockets with Nozzles in Ultra-High-Temperature Ceramic Composites

    7. Comparison of simulation and experimental results for functional verification of a propellant mass-flow regulation device

    8. Development and Qualification of Turbines for the Vinci Upper Stage Engine for Ariane 6

    9. Status of the Turbopump Development in the LUMEN Project

    10. systems advantages of electric pump fed upper stage hybrid rocket

    11. Electrical Pressurization Concept for the Orion-ESM Propulsion System

    12. Development Status of 500 N - class HTP/TMPDA Bi-propellant Rocket Engine

    13. Development of 10N Mark-2 Thruster for Spacecraft Applications

    14. Investigation of New Ignition Systems for Future Launcher Application

    15. Modal Propellant Gauging: High-resolution and non-invasive gauging of both settled and unsettled liquids in reduced gravity.