IP. Interactive Presentations - IAF SPACE TRANSPORTATION SOLUTIONS AND INNOVATIONS SYMPOSIUM

Papers

1. Development of KSLV-II and flight test of its one staged test vehicle employing newly developed main engine(KRE-75)

2. the design and development of a medium-scale liquid commercial launch vehicle named zq-2 based on liquid oxygen and liquid methane propulsion system

3. Multidisciplinary design analysis of a semi-reusable two-stage-to-orbit small payload launch system

4. Lessons and Learns of Launching Test Launch Vehicle of KSLV-II concerning Launch Complex Development

5. Orbit Transfer Analysis with a 3D Vis-Viva Equation

6. Lightning Protection System: current strategy and evolutions

7. suboptimal rocket landing guidance using model predictive static programming

8. Comparative analysis of upper stage and built-in propulsion system for GEO satellite launches

9. Feasibility of an automated streamlined body for launch vehicles and Leo transportation

10. Autophage nanolauncher - a solid SSTO launch vehicle

11. Nanosats and Suborbital Feasible Missions from a Brazilian Launch Center

12. Overview of Avionics Architecture on Stand-alone Test Launch Vehicle (TLV), Second Stage of Korea Space Launch Vehicle-II (KSLV-II)

13. A Study on Mission Design Framework of Reusable Vehicles for Potential Human Spaceflight in LEO

14. Mission Control as a Service - A Turn Key Solution in Space Communications

15. SAAOPL System: Its Design and Technical Feasibility Study

16. Design and development of a Brazilian Liquid Engine Sounding Rocket to Train Launch Operations.

17. Multi-Disciplinary Analysis of Single Stage to Orbit (SSTO):SKYLON Spaceplane

. Guidance system design and verification for the small commercial rocket

. Technical Improvement of Launch Vehicle Control System for Chang'e 4 Mission