Candidates must either have a current Secret clearance or have had a Secret clearance in the last two years
Candidates must be U.S. Citizens
Permanent residents are NOT eligible for this role
Dual citizens are NOT eligible for this role.
Candidates with a current non-U.S. passport in addition to a U.S. passport are NOT acceptable
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.
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.
B.S. degree or higher in Mechanical or Aerospace engineering, or equivalent engineering
17177 PRESTON RD STE 300
DALLAS, TX 75248