rootbrowseIAC-12C2session 77. Space Vehicles – Mechanical/Thermal/Fluidic SystemsPapers1. Recent Thermal Design Driven Development Activities at MT Aerospace2. Cryogenics tasks in perspective Russian scientific space projects3. Coating effects on thermal properties of carbon carbon and carbon silicon carbide composites for space thermal protection systems.4. Chemical non equilibrium simulations of hypersonic flights in carbon dioxide-nitrogen atmospheres using a coupled Euler-second-order boundary layer method5. Re-Use of EXOMARS rover on icy moons of Jupiter6. EXPERT – The ESA Experimental Re-Entry Vehicle: Experiments and Payloads qualified and ready for the flight7. Large Scientific Satellite Tested with Success at LIT-INPE 6m x 8m Space Simulation Chamber8. Uncertainty quantification for hypersonic flow simulations9. Effect of Eccentricity on the Heat Transfer Rates of a Re Entry Vehicle with Concave Windward Surface10. Solid rocket booster segment joint - a parametric study11. Aerothermodynamics of a Hemispherical-Cylindrical Blunt Vehicle with a Flow through Duct12. Robust neural network control of space robot system with flexible joints13. Effect of forebody configuration on nonslender delta wing rock14. Computational analysis of thermal and structural loads on re-entry vehicles and a conceptual SSTO model using an in-house solver code.15. Numerical analysis of engine cylinder liner with inner functionally graded thermal barrier coating16. The Hungarian CoCoRAD experiment in the BEXUS program of the ESA17. Aeroheating and Structure Coupled Analysis in Thermal Protection System for Reusable Launch Vehicle18. Analysis of load transmission line on the fuselage of reusable launch vehicle19. Simulation of multi-body separation of aerospace vehicles based on unstructured overset grids technology20. Correction of Hypersonic Viscous Interaction Correlation Parameter21. An all-speed unstructuredflow solver for separation process22. Numerical simulation of uav carrier-landing interactive flowfield23. Numerical simulation of aerodynamic heating on hypersonic slip flow24. Modeling of hydrogen embrittlement at steady state at high temperature using a commercial finite element program25. Acoustic-elastic of flight vehicle26. Investigate of rudder deflected multi-body separation