rootbrowseIAC-11C2session 77. Space Vehicles – Mechanical/Thermal/Fluidic SystemsPapers1. A new methodology for estimating surface heat flux from in-depth sensors2. Carbon/carbon comparative optimization method for hot structures applications in re-entry environment conditions3. Active thermal control system for perspective venusian lander4. A Thermal Model for Analysis and Control of Drilling in Icy Formations on Mars5. Egse in spacecraft thermal vacuum tests for accurate power measurements and minimization of power supplies6. Application of inertia relief in structural strength analysis of reusable launch vehicle7. RE-USE OF EXOMARS ROVER ON ICY MOONS OF JUPITER8. Versions of orbiters’ flight systems for nonnuclear action on asteroid Apophis9. Spacecraft Aerodynamics and Heat Shield Characteristics Impact on Optimal Aeroassisted Coplanar Orbital Transfer10. Thermal buckling of simply supported moderately thick functionally graded plates11. Research on Flight experiment Technique to Verification Thermal Protection Materials and Insulation Materials12. Application of Structured Singular Value Method to Aeroservoelastic Robustic Stability Analysis for Reusable Launch Vehicle13. Flow-Structure-Thermal Investigation of Blunt Body in High-Enthalpy Flows14. Topological structures and aerodynamic characteristic analysis of hypersonic flow over HTV-type aircraft15. Estimation of crack growth behavior in welded space vehicles structural components16. NUMERICAL SOLUTION OF STEADY VISCOUS FLOW AND HEAT TRANSFER PAST GAS BUBBLES IN A SPACECRAFT HEATPIPE17. Aerothermal computation research for re-entry vehicles in real gas effect18. Research on 3d cavity flow and its aero-optics phenomena19. The numerical study of cone-derived waverider with nonuniform blunt radius20. Cork filled ethylene-propylene-diene monomer based thermal insulation for space vehicles21. Hypersonic surface heating computation on blunt bodies22. Effect of epoxy adhesive on solder joint reliability of 3D Plus SRAM under thermal cycling