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  • session 1
  • 1. Propulsion System (1)

    Papers

    1. The Development Plan of the First and the Second Stage Engines for the Japanese Next Flagship Launch System

    2. Creation of family of LPRE for advanced Russian and foreign launch-vehicles on the basis of RD191 engine

    3. Advancement and Future Application of Space Propulsion Technology Using Hydrocarbon Propellants in China

    4. The Future of Liquid Propulsion: the French view

    5. Results of LE-X engine technology demonstration

    6. VINCI®, the European reference for Ariane 6 upper stage cryogenic engine

    7. Development of a LM10-MIRA LOX – LNG expander cycle Demonstrator engine

    8. firing tests for advanced features and long-life durability of the main engine of the reusable sounding rocket

    9. Applying a Mature Green Propulsion Solution to Enhance Future Mission Capabilities

    10. A Novel Green Gel Propellant Based Propulsion System

    11. Research on thermal decomposition of hydrogen peroxide.

    12. Dynamic characteristics of open-type swirl injector with pulsating manifold pressure

    13. a review of china's lox/kerosene stage combustion cycle rocket engine

    14. Features of the propellant tanks pressurization systems development of the LV upper stages