rootbrowseIAC-22C2session 77. Space Vehicles – Mechanical/Robotic/Thermal/Fluidic SystemsPapers1. Multi-engines cryogenic stage low-cost structures and fluid components for small satellites launch services2. Experimental Validation of a Solid State Magnetocaloric Cooler in a Space Environment3. Analysis of effective thermal control designs for small satellites4. POGO Characteristics and Experimental Analysis of the First Chinese Liquid Oxygen-Methane Launcher “ZQ-2”5. thermal balance and thermal vacuum test of the cbers-4a satellite performed at inpe, brazil.6. EFFECTIVENESS OF A BELLY FLAP IN MARTIAN ATMOSPHERE7. Temperature distribution along a composite and metallic shell in cryogenic environment8. Influence of hydrogen and oxygen self-pressurizing temperature on heat transfer of propellant tank9. Designing the first three-section arm on a CubeSat10. Structural design of a CubeSat type nanosatellite for academic purposes.11. Additively Manufactured High-Power-Density Cold Plates12. The fabrication and application of water sublimator heat dissipation system in Chang'e 5 lunar probe