rootbrowseIAC-17C4session 33. Propulsion Technology (1)Papers1. KEYNOTE: THE AEROJET ROCKETDYNE AR1 STAGED COMBUSTION BOOSTER ROCKET ENGINE2. Ablation experimental characterization and numerical investigation of a 3-dimensionally built carbon/phenolic composite for aerospace applications3. Plume Flow Field Analysis for Lander Propulsion System of Chandrayaan-2 Mission4. Ceramic Catalyst Bed for a Green Liquid Bi-propellant Rocket Engine Using 98% Hydrogen Peroxide as Oxidizer5. optical spectroscopy on laser-induced ignition sparks and other space-relevant plasmas6. experimental investigation of 150n liquid oxygen-liquid methane attitude control engine8. 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 Boosters10. Additive Manufacturing Development for Rocket Engine in Japan11. 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 Propellant13. Comparative analysis regarding usage of different Reaction Control System on microlauncher attitude control14. Green Options for Orbital Propulsion