** Candidates must be U.S. Citizens ** ** Candidates must either have a current Secret clearance or have had a Secret clearance in the last two years. They must be able to obtain and maintain a U.S. Security Clearance at the appropriate level ** ** Must be able to satisfy federal government requirements for access to government information. Permanent residents are not eligible for this role. Dual citizens are not eligible for this role. Also, candidates with a current non-U.S. passport in addition to a U.S. passport are not eligible **
-Conduct aerothermodynamic and heat transfer design and analysis of hypersonic air-breathing propulsion systems (ramjets/scramjets) and/or liquid rocket engines. -Develop thermal models to design and analyze cooled and un-cooled engine components. -Develop fluid flow models using Computational Fluid Dynamics codes or other analytical tools. -Design, test and analyze data from component rigs to supplement or validate analytical models. -Support planning and testing of engines (ground and flight) and analyze the test data. -Document work performed in the form of reports and briefings.
Education: B.S. degree or higher in Mechanical or Aerospace engineering, or equivalent engineering
Skills: -Knowledge of aerothermodynamics and heat transfer as applied to scramjet and/or liquid rocket engine systems, including turbomachinery and combustion devices. -High proficiency levels in ANSYS Mechanical or Workbench heat transfer analysis tools, ANSYS CFX, FLUENT or comparable CFD codes.
12 - months
11100 NE 8TH ST STE 800
BELLEVUE, WA 98004