This role supports new aircraft program development and in-service aircraft for all thermodynamics-related issues. This includes performance of aircraft ice/fog protection systems, zonal pressure, temperature and flow rate analysis, avionics cooling, and general thermal analysis of systems and structures. The position requires an understanding of the systems being analyzed and their interfaces with the aircraft and other aircraft systems. It also involves communication with internal systems/structures groups, system suppliers, and flight test teams to resolve issues, plan tests, analyze, and certify modifications. Specifically, this position will assist the Global 7000/8000 thermodynamic team with activities related to bleed air systems, such as wing ice protection systems, environmental control systems, and ducting systems.
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Job Type
Full-time
Career Level
Mid Level