rootbrowseIAC-16C4session 11. Propulsion System (1)Papers1. KEYNOTE: Additive Layer Manufacturing will change rocket liquid propulsion2. overview of le-9 engine development for h3 launch vehicle3. VULCAIN 2.1®, the European reference for Ariane 6 Lower stage cryogenic engine4. LOX/METHANE reusable rocket propulsion at reach with large scale demonstrators tested5. Effect of bearing supporting stiffness on critical speed and dynamic stability of turbo-pump rotor system in LOX/Kerosene rocket engine6. Challenges in restart of pressure fed liquid upper stage7. Leveraging Additive Manufacturing for Affordable Commercial Launch Applications Enabled by the Aerojet Rocketdyne Ultra-Low-Cost Bantam Engine Family8. Vinci® Propulsion System: Transition from Ariane 5 ME to Ariane 69. Development of an up-rated version of earth storable pump fed liquid engine for ISRO launch vehicles.10. static characteristic analysis of 180kn lox/kerosene upper stage engine11. Development status of CE20 cryogenic engine for GSLV LVM3 vehicle12. Multidiscipline approach to the design and modernization of high power Liquid Propellant Engines for their reuse13. effect of fuel injection schemes in a vortex combustion chamber14. The design and test of 250N thruster with HAN-based propellant15. Multidisciplinary design optimization of a spacecraft bi-propellant propulsion system using a computationally improved framework