rootbrowseIAC-20C2session 77. Space Vehicles – Mechanical/Robotic/Thermal/Fluidic SystemsPapers2. Application of Magnetocaloric Cooling Components for Small Satellite Systems4. Flexible and Scalable Thermal Design of Modular On-Orbit Assembly Microsatellite5. DIAGNOSTICS OF DEFECTS OF THERMAL PROTECTIONS INFLATABLE RE-ENTRY VEHICLES7. Thermal Analysis and TVAC Testing of the Hope Probe (Emirates Mars Mission)9. Attitude control system of a microsatellite based on the inverse problems technique and the Kalman filter10. Reliability-based multi-objective design optimization of the satellite thermal control system using swarm-based optimization algorithms12. Development of a thermal design model for a small spacecraft with integrated heat pipes13. MONITORING AND ANALYSIS OF THE STRESSED-DEFORMED CONDITION OF THE SHELLS, IN THE PROCESS OF THEIR MANUFACTURE DURING 3D PRINTING AND WELDING WORKS15. Cooling Channel at the Leading Edge of Supersonic Vehicle design based on Working fluid convection16. SharjahSat-1 Thermal Analysis for Orbit-Launch Selection