f7d8749a-72d6-407c-bf98-292ea630c73a Senior Flight Sciences Engineer at Shield AI specializing in aeropropulsion integration and performance modeling. Support design, testing, and flight of unmanned aircraft propulsion systems.
Responsibilities
As a Senior Flight Sciences Engineer focused on aeropropulsion, you will work across disciplines to enable the design, build, test, and flight of high performance unmanned aircraft. The Flight Sciences team encompasses aerodynamics, aircraft performance, aeropropulsion, stability and control, aerodynamic modeling, wind tunnel testing, and flight testing. Within this team, you will focus on how the propulsion system and airframe work together, including inlet and exhaust design, installed propulsion performance, and propulsion airframe integration.
This role is perfect for an engineer with a solid foundation in aerodynamics, propulsion, or flight sciences who is eager to grow, own challenging projects, and see their work move rapidly from concept to flight. If you thrive in fast paced environments, enjoy solving complex problems, and want to help build the future of autonomous aviation, we want to hear from you.
Support aeropropulsion design from the conceptual phase through flight, including inlet, duct, nozzle, and exhaust system definition
Develop installed propulsion performance models, including inlet pressure recovery, distortion, spillage drag, nozzle performance, and installed thrust for Shield’s latest unmanned aircraft
Analyze propulsion airframe integration effects, including thrust and drag bookkeeping, inlet and engine compatibility, and propulsion induced effects on aircraft performance and stability
Contribute to flight sciences support through flight test data analysis, ducted fan and propulsion performance modeling, and correlation of models to test results
Collaborate with propulsion, structures, flight test, and control systems engineers to ensure integrated, optimized, and safe aircraft performance
Support wind tunnel, propulsion ground test, and flight test events, including test planning, instrumentation requirements, and data reduction
Qualification
Working understanding of gas turbineTemporary employee offer package
Required
B.S. in Aerospace or Mechanical Engineering or equivalent
3 or more years of experience in aeropropulsion, propulsion integration, aerodynamics, aircraft performance, or flight sciences
Working understanding of gas turbine, ducted fan, or propeller performance and installation effects on aircraft performance
Demonstrated record of working hard and being a trustworthy teammate
Preferred
Experience with computational fluid dynamics for inlet, nozzle, ducted fan, or internal flow analysis
Experience with engine performance decks, cycle analysis tools such as NPSS, or propulsion system modeling
Experience with inlet or propulsion wind tunnel testing, engine ground testing, or propulsion flight test
Experience scripting or developing software in Python, MATLAB, or similar languages
Experience with analysis of large data sets
Full-time regular employee offer package:
Pay within range listed + Bonus + Benefits + Equity