Engineer VI
General Atomics - Location not specified
Posted Jun 10, 2026
Benefits
- Parental leave
- Not verified
- Non-birth-parent leave
- Not verified
- Family-building benefits
-
- Fertility benefits: Not verified
- Adoption assistance: Not verified
- Surrogacy assistance: Not verified
- Mental health support
- Not verified
- Relocation assistance
- Not verified
- Childcare support
- Not verified
- Learning budget
- Not verified
- Verification
- Not verified checked Jun 7, 2026
- Salary
- Not verified
- 401(k) match
- Reported from DOL Form 5500 industry filing (not employer-specific)
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Market context
- U.S. role benchmark (BLS OEWS)
- $116,543 U.S. median for this role
- Projected growth (BLS Employment Projections)
- +9.8% - Much faster than average
Matched to SOC 15-1252 - Software Engineering aggregate by role bucket.
Source: U.S. Bureau of Labor Statistics, OEWS, May 2024 and Employment Projections, 2024-2034.
Role
Schedule
- Shift type
- Not verified
- Weekend work
- Not verified
Application
- Cover letter
- Not verified
- Assessment
- Not verified
- Deadline
- Not stated
Where they hire
State eligibility is not yet verified.
About this role
Engineer VI General Atomics Aeronautical Systems, Inc. (GA-ASI), an affiliate of General Atomics, is a world leader in proven, reliable remotely piloted aircraft and tactical reconnaissance radars, as well as advanced high-resolution surveillance systems. We have an exciting opportunity in San Diego, CA (Poway, CA) for a Senior Loads and Dynamics Engineer in our Airframe Integrity Group. Under general supervision with limited review, this position is responsible for determining and developing effective approaches for resolving a wide range of difficult engineering problems. DUTIES AND RESPONSIBILITIES: - Responsible for supporting the design of new products, expanding capability to existing products, and integrating new payloads onto existing platforms. - Responsible for performing loads and dynamics analysis of aircraft components, assemblies, and systems. - Develop design and repeated loads for air vehicle flight, landing, and ground operations. - Flight Loads analysis includes the development of open and closed loop aeroelastic flight loads models, the calculation of aerodynamic and inertial loads across the aircraft. - Landing and Ground loads includes hand calculation methods, structural dynamics and explicit simulations of landings. - Dynamics analysis includes normal modes, frequency response, random vibration, and the development of vibration and shock environmental criteria. - Develop aeroelastic models for use in flutter and aeroservoelastic analysis. - Utilize ground vibration test data to correlate structural dynamics models. - Perform analysis by way of classical and computer methods, and develop new methodologies for load development. - Generate documentation to support design and airworthiness certification using MIL, STANAG, or FAR standards. We
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