About this role
<p><em><span style="font-size:14.0pt"><span style="font-family:Verdana, Geneva, sans-serif"><strong><span style="color:black">Job Title: Sr Specialist, Structural Engineer</span></strong></span></span></em></p> <p><em><span style="font-size:14.0pt"><span style="font-family:Verdana, Geneva, sans-serif"><strong><span style="color:black">Job Code: 33382</span></strong></span></span></em></p> <p><em><span style="font-size:14.0pt"><span style="font-family:Verdana, Geneva, sans-serif"><strong><span style="color:black">Job Location: Huntsville, AL </span></strong></span></span></em></p> <p><span style="font-size:14.0pt"><span style="font-family:Verdana, Geneva, sans-serif"><strong><span style="color:black"><em>Job Schedule: 9/80: Employees work 9 out of every 14 days – totaling 80 hours worked – and have every other Friday off </em></span></strong></span></span></p> <p> </p> <p><span style="font-size:14.0pt"><span style="font-family:Verdana, Geneva, sans-serif"><strong><span style="color:black">Job Description:</span></strong></span></span></p> <p> </p> <p><span style="font-size:14.0pt"><span style="font-family:Verdana, Geneva, sans-serif">In this role, you will perform structural analysis to verify product designs meet structural performance requirements and assist with preliminary design verification. This role requires an experienced structural engineer with a strong technical foundation in aerospace structures, particularly rocket propulsion, a proactive mindset, and a passion for solving problems that can be but are not typically complex in high-performance environments. </span></span></p> <p> </p> <p><span style="font-size:14.0pt"><span style="font-family:Verdana, Geneva, sans-serif">As a key contributor, you will manage and/or support structural modeling and analysis efforts for solid rocket motor (SRM) components throughout the product lifecycle—from early development through qualification and production. You will collaborate closely with cross-disciplinary teams, interface with customers, and drive technical excellence. Work will be performed under general oversight.</span></span></p> <p><span style="font-size:14.0pt"><span style="font-family:Verdana, Geneva, sans-serif"> </span></span></p> <p><span style="font-size:14.0pt"><strong>Why This Role Matters</strong>:</span><br><span style="font-size:14.0pt">You won’t be just running models - you’ll be influencing major design decisions and contributing directly to flight-critical hardware. This position is a unique opportunity to work on cutting-edge propulsion technologies that drive national defense initiatives.</span></p> <p> </p> <p><span style="font-size:14.0pt"><span style="font-family:Verdana, Geneva, sans-serif"><strong><span style="color:black">Essential Functions:</span></strong></span></span></p> <p> </p> <ul style="margin-bottom:11.0px"> <li style="font-size:14.0pt"><span style="font-size:14.0pt"><span style="font-family:Verdana, Geneva, sans-serif"><strong>Structural Analysis Ownership</strong>: Drive analysis tasks for SRM components including metallic and composite motor cases, nozzles, insulation, and propellant grains. Ensure structural integrity across all phases of flight and ground handling.</span></span></li> <li style="font-size:14.0pt"><span style="font-size:14.0pt"><span style="font-family:Verdana, Geneva, sans-serif"><strong>FEA Modeling & Execution</strong>: Build and execute finite element models using ANSYS, ABAQUS, or comparable tools. Model components using isotropic, orthotropic, and viscoelastic material definitions with nonlinear and temperature-dependent properties.</span></span></li> <li style="font-size:14.0pt"><span style="font-size:14.0pt"><span style="font-family:Verdana, Geneva, sans-serif"><strong>Load Development</strong>: Collaborate with thermal, CFD, and performance teams to establish pressure, thermal gradient, and mechanical loading conditions. In some cases, derive boundary conditions and load cases based on mission and design requirements.</span></span></li> <li style="font-size:14.0pt"><span style="font-size:14.0pt"><span style="font-family:Verdana, Geneva, sans-serif"><strong>Closed-Form Support</strong>: Apply classical methods to validate and supplement numerical results, especially for preliminary design trades or quick-turn assessments.</span></span></li> <li style="font-size:14.0pt"><span style="font-size:14.0pt"><span style="font-family:Verdana, Geneva, sans-serif"><strong>CAD & Geometry Integration</strong>: Import and simplify solid CAD models from design teams to develop robust, clean geometry suitable for analysis.</span></span></li> <li style="font-size:14.0pt"><span style="font-size:14.0pt"><span style="font-family:Verdana, Geneva, sans-serif"><strong>Margin of Safety Evaluation</strong>: Determine margins of safety against yield, ultimate failure, buckling, HCF, LCF, and fracture using established industry standard practices and internal allowables.</span></span></li> <li style="font-size:14.0pt"><span style="font-size:14.0pt"><span style="font-family:Verdana, Geneva, sans-serif"><strong>Documentation & Reporting</strong>: Produce high-quality technical reports, stress notes, and presentations that clearly outline methods, assumptions, and conclusions for both internal reviews and external customer delivery.</span></span></li> <li style="font-size:14.0pt"><span style="font-size:14.0pt"><span style="font-family:Verdana, Geneva, sans-serif"><strong>Design Integration</strong>: Participate in formal and informal design reviews. Communicate results, trade-offs, and risk areas effectively to multidisciplinary audiences, including program management and external customers.</span></span></li> <li style="font-size:14.0pt"><span style="font-size:14.0pt"><span style="font-family:Verdana, Geneva, sans-serif"><strong>Process Improvement</strong>: Contribute to internal tool development, analysis automation, and knowledge capture to enhance team efficiency and standardization.</span></span></li> <li style="font-size:14.0pt"><span style="font-size:14.0pt"><span style="font-family:Verdana, Geneva, sans-serif"><span style="color:black">Ability to obtain a US Security Clearance.</span></span></span></li> </ul> <p> </p> <p><span style="font-size:14.0pt"><span style="font-family:Verdana, Geneva, sans-serif"><strong><span style="color:black">Qualifications:</span></strong></span></span></p> <p> </p> <ul style="margin-bottom:11.0px"> <li style="font-size:14.0pt"><span style="font-size:14.0pt"><span style="font-family:Verdana, Geneva, sans-serif">Bachelor’s Degree and minimum 6 years of prior structural analysis experience. </span>Graduate Degree and a minimum of 4 years of prior <span style="font-size:14.0pt"><span style="font-family:Verdana, Geneva, sans-serif">structural <span style="font-size:14.0pt">analysis</span></span></span> experience. <span style="font-family:Verdana, Geneva, sans-serif">In lieu of a degree, minimum of 10 years of prior <span style="font-size:14.0pt">structural <span style="font-size:14.0pt">analysis </span></span>experience.</span></span></li> </ul> <p> </p> <p><span style="font-size:14.0pt"><span style="font-family:Verdana, Geneva, sans-serif"><strong><span style="color:black">Preferred Additional Skills:</span></strong></span></span></p> <p> </p> <p> </p> <ul> <li style="font-size:14.0pt"><span style="font-size:14.0pt">Bachelor’s Degree (in Mechanical, Aerospace, or related Engineering discipline) is preferred.</span></li> <li style="font-size:14.0pt"><span style="font-size:14.0pt">Master’s degree preferred.</span></li> <li style="font-size:14.0pt"><span style="font-size:14.0pt">Proven experience in linear, nonlinear, and dynamic structural analysis supporting design and qualification of solid rocket motors.</span></li> <li style="font-size:14.0pt"><span style="font-size:14.0pt">Proficiency with FEA tools such as <strong>ANSYS Mechanical</strong>; experience with <strong>ANSYS MAPDL</strong> or<strong> Python</strong> scripting is highly desirable.</span></li> <li style="font-size:14.0pt"><span style="font-size:14.0pt">Familiarity with structural assessment and design of filament-wound composite pressure vessels is a strong asset.</span></li> <li style="font-size:14.0pt"><span style="font-size:14.0pt">Demonstrated ability to interpret aerospace structural requirements and coordinate load development with cross-functional teams.</span></li> <li style="font-size:14.0pt"><span style="font-size:14.0pt">Working knowledge of structural instabilities, material nonlinearities, and coupled load environments.</span></li> <li style="font-size:14.0pt"><span style="font-size:14.0pt">Exposure to full lifecycle aerospace <strong>SRM propulsion</strong> product development, from design through manufacturing and test.</span></li> <li style="font-size:14.0pt"><span style="font-size:14.0pt">Strong technical communication skills and proficiency with Microsoft Office (Word, Excel, PowerPoint).</span></li> </ul> <p><span style="color:white;font-size:14.0pt">#LI-HW1</span></p> <p> </p>