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  • session 7
  • 7. Space Vehicles – Mechanical/Thermal/Fluidic Systems

    Papers

    1. CDR-Level Structural Modelling And Optimization Of The Mercury Sodium Atmosphere Spectral Imager (MSASI)

    2. computational fluid dynamics analysis and flow test of manned spacecraft

    3. COMPUTATIONAL MODELLING OF HEAT TRANSFER IN A SPACECRAFT HEAT PIPE.

    4. Coupled aeroassisted orbital plane change manoeuvre and thermal protection system optimization

    5. Destructive materials thermal properties determination with application for spacecraft structures testing

    6. enabling technologies for hot structures of next generation rlv's - the asa program summary

    7. Experimental and Numerical Studies of Spallation Particles Ejected from a Light-weight Ablator

    8. effective parameters on calculation of effective thermal conductivity of multilayer printed circuit boards in space application

    9. IBDM: The International Berthing Docking Mechanism For Human Missions to Low Earth Orbit and Exploration

    10. Optical sensor system applicability for spacecraft tests

    11. Research on the thermal control hardware combined with heat pipe and phase change material

    12. Surface Heat Flux Estimation and New Calibration Methods For Ground-Based Testing in Hypersonic Environments

    13. Wing Leading Edge Ablation Tests in Arc Tunnel

    14. results from the thermal balance testing of the cbers 3-4 satellite tm