rootbrowseIAC-18C2session 77. Space Vehicles – Mechanical/Thermal/Fluidic SystemsPapers1. Automated Thermal Model Correlation Tool for Space Applications2. Optimum Design and Thermal Analysis of Composite Insulation Structure Used in Cryogenic Storage Tanks on-orbit3. Micro-pumped cooling loop to standardize micro-sat thermal control4. A backup system of a satellite orientation based on inverse problems technique5. Evaluation of thermal analysis of orbital environment of microsatellite ALE-16. The way of defining a powerful method for supersonic and hypersonic winged spacecraft aerodynamics prediction7. Thermal Loads Simulators and Setup Strategies of Thermal Tests for Small Satellites8. Unsteady Coupled Heat Transfer Simulations of Hypersonic Gap Flows9. Using the “Comparative Test Method” to Determine the Heat Statuses for the Heat Shields of Spacecraft10. Experimental and Numerical Study on the PCM Thermal Control Device for Spacecraft Electronics11. Thermal Control of High Power Applications on CubeSats12. The Influence of Shock Wave on Ablation Thermal Environment of Re-entry Vehicle Protuberance