rootbrowseIAC-19C4session 22. Propulsion System (2)Papers1. KEYNOTE: OmegA Launch Vehicle2. Ariane 6 and Vega-C programs: the P120C SRM nozzle qualification3. Performance evaluation of 4D Carbon-Carbon throat insert through Hot test of Solid Motor4. Design and Developmental Challenges of Slow Burning Solid Booster for Sub-orbital Hyper Sonic re-entry Experiment5. Performance and environmental impact prediction of SRMs. Road map for reliable dataset of particles in plume6. Analysis of Solid Propellant Combustion Using Image Processing Techniques7. Mars Ascent Vehicle (MAV) Preliminary Architecture Assessment Overview8. A Study on New Hybrid Rocket Engine with Multi-Section Swirl Injection and Aft Counter-Swirl Injection Method9. Real-time regression rate measurement of an additive-manufactured functional hybrid rocket fuel10. Cost-Effective Hybrid Rocket Launch Vehicle of Taiwan11. Green Fuels for Rocket Propulsion: Current Status and Future Perspectives of Paraffin-based Formulations12. dynamic response of thrust modulation in hybrid rocket for VTVL propulsion system13. Performance Analysis of N2O/CO2 Oxidizer Mixture with Paraffin based Micro-Aluminum Fuel for Mars Ascent Vehicles. Analysis and experiments considering 98%+ Hydrogen Peroxide hybrid rocket motors with additive manufactured fuel grains