rootbrowseIAC-10C2session 77. Space Vehicles – Mechanical/Thermal/Fluidic SystemsPapers1. CDR-Level Structural Modelling And Optimization Of The Mercury Sodium Atmosphere Spectral Imager (MSASI)2. computational fluid dynamics analysis and flow test of manned spacecraft3. COMPUTATIONAL MODELLING OF HEAT TRANSFER IN A SPACECRAFT HEAT PIPE.4. Coupled aeroassisted orbital plane change manoeuvre and thermal protection system optimization5. Destructive materials thermal properties determination with application for spacecraft structures testing6. enabling technologies for hot structures of next generation rlv's - the asa program summary7. Experimental and Numerical Studies of Spallation Particles Ejected from a Light-weight Ablator8. effective parameters on calculation of effective thermal conductivity of multilayer printed circuit boards in space application9. IBDM: The International Berthing Docking Mechanism For Human Missions to Low Earth Orbit and Exploration10. Optical sensor system applicability for spacecraft tests11. Research on the thermal control hardware combined with heat pipe and phase change material12. Surface Heat Flux Estimation and New Calibration Methods For Ground-Based Testing in Hypersonic Environments13. Wing Leading Edge Ablation Tests in Arc Tunnel14. results from the thermal balance testing of the cbers 3-4 satellite tm