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Space Dynamics Laboratory

Nonprofit laboratory for space and defense research

Mechanical Engineer

Materials & StructuresConfirmed live in the last 24 hours
Full-timeNorth Logan, UT, USA$88k - $180k /yr

About the Job

Requirements

  • A bachelor's degree in mechanical engineering, aerospace engineering, or a closely related technical field is required.
  • At least five years of relevant structural analysis experience is required; equivalent demonstrated technical responsibility may be considered.
  • Proficiency in finite element analysis software such as FEMAP/NASTRAN, ANSYS, Abaqus, or equivalent, with the ability to independently develop and critically evaluate models, is required.
  • Experience with static structural analysis and structural dynamics, including modal analysis and vibration response, is required; experience with aerospace or similarly demanding hardware is relevant.
  • Ability to calculate and substantiate structural margins of safety and independently check results using sound engineering fundamentals is required.
  • Experience supporting structural or environmental testing and evaluating test results is required.
  • Ability to interpret engineering drawings and CAD models and provide structural design-review feedback is required.
  • Experience documenting technical analyses, plans, procedures, and results and presenting conclusions to multidisciplinary teams is required.
  • Ability to work effectively across engineering disciplines and communicate technical assumptions, uncertainties, and recommendations is required.
  • Must have or be able to obtain a Department of War security clearance and must be a U.S. citizen.
  • Must be able to travel regularly and support off-site work for extended periods when required by project needs.

Responsibilities

  • Perform static, quasi-static, modal, random-vibration, and other applicable structural analyses of spacecraft, optical payloads, components, and mechanical interfaces.
  • Develop, validate, and interpret finite element models; establish realistic loads, boundary conditions, connections, load paths, and mesh convergence; and corroborate results with first-principles calculations.
  • Calculate and document structural margins of safety for applicable strength, stiffness, stability, fatigue, fastener/joint, and other relevant failure modes using approved requirements and material properties.
  • Review 3D mechanical designs and engineering drawings for structural adequacy, interface compatibility, materials, tolerances, and fabrication-related structural risks, and collaborate with designers on improvements. CAD modeling and drawing release are not primary duties.
  • Prepare structural analyses, design trades, verification plans, technical reports, and presentations for PDR, CDR, and other formal reviews.
  • Develop structural test predictions; support static, modal, vibration, and shock qualification tests as applicable; evaluate test results, correlate models, and help resolve anomalies.
  • Work with laboratory, fabrication, procurement, program management, systems, optical, and thermal teams to support hardware build, integration, and delivery.
  • Manage assigned analysis scope, schedule, and technical deliverables; mentor or review the work of other engineers as appropriate to experience level.

Desired Qualifications

  • A master's degree in mechanical engineering, aerospace engineering, or a related field, and 10 or more years of directly relevant experience.
  • Ownership of spacecraft or optical-payload structural verification through PDR/CDR, fabrication, integration, environmental qualification, and delivery.
  • Proficiency with FEMAP, HyperMesh, and MSC/Siemens NASTRAN, including dynamic analysis, stress recovery, and model correlation.
  • Experience with random-vibration PSD analysis, sine vibration, modal survey, shock response, coupled-loads analysis, and launch environments.
  • Experience with fatigue, fracture, buckling, nonlinear contact, thermal stress, and bonded or bolted joint analysis, including NASA-STD-5020 methods.
  • Experience with composite structures, sandwich panels, inserts, adhesive joints, and composite failure criteria.
  • Experience reviewing precision optomechanical designs, flexures, mechanisms, and dimensional-stability requirements; familiarity with STOP analysis.
  • Experience with structural qualification test planning, instrumentation, test-data reduction, and test/analysis correlation.
  • Familiarity with Siemens NX or equivalent CAD for model inspection and drawing review; CAD production responsibility is not expected.
  • Experience with Python, MATLAB, or similar tools for analysis automation and test-data processing.
  • Experience with space-environment design and relevant NASA, Department of Defense, or ECSS structural verification practices.
  • Active TS/SCI security clearance.

About the Company

Space Dynamics Laboratory

Nonprofit laboratory for space and defense research

Space Dynamics Laboratory develops satellites, sensors and mission software for national defense, space exploration and scientific research. The nonprofit research corporation is wholly owned by Utah State University and operates as a university affiliated research center sponsored by the US Space Force. Its teams design and build instruments and spacecraft, test them for flight and develop ground systems that process mission data. Work spans government research partnerships and engineering programs, with support from initial mission concepts through deployment. The laboratory's operating roots date to 1959, and it took its present form through a 1982 merger; its headquarters are in North Logan, Utah.

Company size
1,001-5,000
Company stage
Not listed
Total funding
Not listed
Headquarters
North Logan, UT
Founded
1959

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