Experience in the design, assembly, testing, certification, and operation of space ATCS systems and components, which may include but not be limited to pumps and valves, coolant loops, cold plates, heat exchangers, sublimators, radiators, and heat exchangers during pre-launch, flight, and post-landing phases. The Systems Engineer, ATCS will: Review system architectures, hardware requirements, designs, assembly procedures, test plans, procedures and data of ATCS for Commercial vehicles and US Deorbit Vehicle (USDV) modules to ensure approaches are sound, component/material selection is appropriate for the intended usage, and suitable for the proposed application.