rootbrowseIAC-19C2session 77. Space Vehicles – Mechanical/Robotic/Thermal/Fluidic SystemsPapers1. Boundary Layer Stability and Laminar-Turbulent Transition Analysis with Thermochemical Nonequilibrium Applied to Martian Atmospheric Entry2. INPPS Flagship with iBOSS Building Blocks3. Evaluating the Feasibility of Smart Radiator Device (SRD) through Simulated Small Satellite Missions4. Why Did NASA Limit the Use of Magnesium? Flammability and Corrosion Testing of Lightweight Magnesium Alloys for Space Flight Hardware Applications5. Proposition of application of Generative Design algorithms in thermal apparatus design and calculations6. Diagnostics of defects of thermal protections inflatable re-entry vehicles7. DYNAMIC STALL CHARACTERISTICS OF LOW REYNOLDS NUMBER AIRFOIL IN MARTIAN AND TITAN’S ATMOSPHERE8. thermal design strategy utilizing transformable structure of spacecraft9. simulation of rarefied hypersonic flows by using the direct simulation monte carlo method10. Qualification of an Infrared Array Based on NiCr Strips for CBERS 4A Satellite’s Space Simulation Test11. RUAG’s development of a modular low-shock jettison system12. Suitability of Manufacturing Processes for In-Space Manufacturing of Spacecraft Components. Aerodynamic Database Design and Flight Data Analysis of a Waverider Vehicle. Calculating detection of flow’s gas dynamic parameters leap by method of tracking zones.