rootbrowseIAC-13D2session PP. Poster SessionPapers1. Experimental study on the high-pressure gas flow performance of orifice plates used in the rocket propellant pressurization system2. visualization technology of numerical simulation for launch vehicle during flight3. a possibility based mission design optimization for the space launch vehicle4. Experimental Research on Simulation of Rockets Takeoff5. A New Optics and Radar Strap-down Measuring System6. Research on Fast Testing Methos of Launch Vehicle7. Adaptive Fault-tolerant Control System of Reusable Launch Vehicle8. development of a linear sweeping frequency pressure generator for dynamic pressure calibration9. water suppression test on jet noise10. Stable tracking of Narrow-beam Instrumentation Radar of Space Tracking Ship11. An analytical for the designing of general assembly-test building of spacecraft launch site12. the analysis about the developing approaches of technologies of safely recycling and reusing launch vehicle core stages and rocket boosters13. Aerodynamic analysis of the USV3 vehicle from hypersonic to landing flight conditions14. Orbital transfer transport system base on upper stage technology15. Multi-disciplinary design and trajectory optimisation of a Single-Stage-to-Orbit Vehicle16. FEASIBILITY STUDY OF SPACECRAFT CLUSTER LAUNCHES WITH ONE LAUNCH VEHICLE INTO VARIOUS BASIC ORBITS17. Rockoon LEEM Project18. A Framework for Integrating Different Space Launch Concepts for Efficient Space Launch Operations19. the solution of future space transport—the patent analysis of 3dp technology application in aerospace20. Aerothermodynamics of round leading edge airfoil with a flow-through duct at hypersonic speed21. Vacuum Maglev - a greener and sustainable space transport system that could kick-start further international collaboration.22. Research on the Integration of Small Launch Vehicle and Small Satellite Platform23. A Balloon Based Launch System for Micro/Nano/Pico-Satellites24. The Control System Simulation of New Launch Vehicle Based on HLA25. Manned Lunar Launching Mode and the Requirement for Heavy LAUNCH Vehicle26. study of a new aerospace vehicle project based on turbine-based combined cycle engine