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  • session 3
  • 3. Propulsion Technology (1)

    Papers

    1. KEYNOTE: THE AEROJET ROCKETDYNE AR1 STAGED COMBUSTION BOOSTER ROCKET ENGINE

    2. Ablation experimental characterization and numerical investigation of a 3-dimensionally built carbon/phenolic composite for aerospace applications

    3. Plume Flow Field Analysis for Lander Propulsion System of Chandrayaan-2 Mission

    4. Ceramic Catalyst Bed for a Green Liquid Bi-propellant Rocket Engine Using 98% Hydrogen Peroxide as Oxidizer

    5. optical spectroscopy on laser-induced ignition sparks and other space-relevant plasmas

    6. experimental investigation of 150n liquid oxygen-liquid methane attitude control engine

    8. Technology Development of an Electrically Driven Pump Fed Storable Liquid Bi-Propellant for a Mars Ascent Vehicle.

    9. Trade-off Study and Thruster System Test of Reaction Control System for Reusable Rocket Boosters

    10. Additive Manufacturing Development for Rocket Engine in Japan

    11. Test of flow deflector proof-of-concept models in LOX/Methane combustion gases.

    12. A Study on the Condensed Primary Combustion Products of Boron-based Fuel-rich Propellant

    13. Comparative analysis regarding usage of different Reaction Control System on microlauncher attitude control

    14. Green Options for Orbital Propulsion