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Aerospace Structural Engineer

Collier Aerospace · Raleigh, NC, United States · On Site · Active · Rippling ATS

Job facts

FieldValue
CompanyCollier Aerospace
TitleAerospace Structural Engineer
Normalized title-
Department / teamEngineering Services
LocationRaleigh, NC, United States
Work modelOn Site
Employment typeFull Time
Salary-
Statusactive
ATS providerRippling ATS
Posted / first seen2025-09-30 / 2026-05-29
Changed / last seen2026-06-23 / 2026-06-23

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Company jobsActive postings from Collier Aerospace.Open
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ATS provider jobsActive postings observed through Rippling ATS.Open
Provider filtered searchThe same provider as a filtered job collection.Open
City jobsActive postings in Raleigh.Open
Department jobsActive postings in Engineering Services.Open
Work model jobsActive On Site postings.Open
Lifecycle eventsOpen, update, close, and reopen events for this posting.Open
Original postingCanonical source or apply URL captured from the ATS.Open

Linked records

CompanyCollier Aerospace
Source4c4042bb-39e7-4fd9-9845-078a573780cd
ATS providerRippling ATS

Description

company Our Why At Collier Aerospace, our mission is to help our customers reach their unique structural analysis and design goals with more accurate results in less time. We are a team of passionate employees who want to contribute to each customer's goal in the best way possible across space launch, reusable rocket, commercial airframe, business jet, eVTOL, bike frame, and speed boat applications. We accomplish this with our leading software, HyperX, through software development and engineering support. As you join our team, you join our company mission and become an integral partner in increasing efficiency and innovation throughout the world. Our Culture We foster a highly supportive and collaborative environment where our meetings are a mix of brainstorming, analysis, and humor. When you’re stuck, our employees are always eager to lend a helping hand. We offer a relaxed and casual dress code to promote a comfortable atmosphere. Our passion and drive fuel us as we strive to make a lasting impact on our company, customers, and industry. role Requirements Candidates should have comprehensive experience in performing aerospace structural stress analysis and design. The candidates should have many of the following capabilities: Bachelor’s Required; Master’s Preferred (0-2) years’ experience – entry level Following aerospace industry practices, capability to perform structural analysis and design with composite materials. Additionally experience with metals a plus. Understanding of overall load paths and an intuitive feel for the efficient use of structural concepts and materials. Experience performing classical hand stress analysis and finite element analysis (FEA) with either Nastran/Abaqus/Optistruct; FEM meshers Hyperworks/FEMAP/Ansa; and a plus to have CAD competence with Catia/3DX/NX. Proficiency in applying appropriate failure theories, preparing structural analysis reports, and identifying critical load conditions and margins-of-safety. Knowledge of panel buckling, local buckling, crippling, and material strength as well as classical in-plane laminate stress analysis. Experience with both ply based (max strain, Tsai-Wu) and laminate based (AML, polynomial) strength prediction approaches and associated material allowables, including damage. Experience with analysis of composite fasteners for bearing and bypass, and bonded joints for out-of-plane interlaminar shear and peel stress analysis, or residual strength energy solutions. Experience sizing structures for minimum weight and practical design experience of composite laminates, including ply drop ratios and layup patterns on complicated surfaces, such as padups around cutouts and bolted joints. Strong documentation, communication, and presentation skills. US Citizen. Roles and Responsibilities Ability to learn and use HyperX for preliminary and detail analysis/design sizing optimization of full airframe and space vehicles. Candidates must be adept at using engineering software tools, learning new software and analysis methods, and working in a Windows OS environment. Use HyperX and other software tools to analyze and design customer airframes and space launch vehicles. Perform trade studies for weight savings and part producibility. Perform both preliminary and detail design and analysis. Document design and analyses results. Candidates will be reporting directly to NASA and industry OEM customers and must be able to verify and describe the application of external loadings and their resolution into critical internal mechanical and thermal load paths, and to the resulting optimum design and their margins of safety. Ensure project issues are resolved in a timely fashion with your related experience and competence and an ability to create workaround procedures when needed. Escalate urgent problems requiring more in-depth knowledge to appropriate engineering leads. Participate in overall HyperX software testing and provide your suggestions to development and modification of the software. Benefits Competitive salary and benefits (PTO, 401(k), health insurance, HSA/HRA eligibility, life and disability insurances) Exposure and involvement with many companies and their current aircraft designs (commercial transports/UAM eVTOLS/military planes) and space launch designs (commercial rockets/space tourism vehicles/demonstrator X planes) Occasional travel to customer facilities Small company, large impact Passionate coworkers Company events and conferences

Full job record

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Org ID9f91f6c2-86ba-422d-b262-81658ea68dc3
Source ID4c4042bb-39e7-4fd9-9845-078a573780cd
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TitleAerospace Structural Engineer
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Location TextRaleigh, NC, United States
DepartmentEngineering Services
Team
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Remote Policy
CountryUnited States
RegionNC
CityRaleigh
Salary Raw
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Salary Currency
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First Seen At2026-05-29 07:15:01Z
Last Seen At2026-06-23 09:06:38Z
Last Checked At2026-06-23 09:06:38Z
Last Changed At2026-06-23 09:06:38Z
Inactive At
Source Posted At2025-09-30 16:58:07Z
Source Updated At
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Experience with both ply based (max strain, Tsai-Wu) and laminate based (AML, polynomial) strength prediction approaches and associated material allowables, including damage.</span></li><li style=\"font-size:12pt;margin:3px 0px;letter-spacing:0.25px;line-height:1.6;\"><span style=\"font-size:12pt;white-space:pre-wrap;\">Experience with analysis of composite fasteners for bearing and bypass, and bonded joints for out-of-plane interlaminar shear and peel stress analysis, or residual strength energy solutions.</span></li><li style=\"font-size:12pt;margin:3px 0px;letter-spacing:0.25px;line-height:1.6;\"><span style=\"font-size:12pt;white-space:pre-wrap;\">Experience sizing structures for minimum weight and practical design experience of composite laminates, including ply drop ratios and layup patterns on complicated surfaces, such as padups around cutouts and bolted joints.</span></li><li style=\"font-size:12pt;margin:3px 0px;letter-spacing:0.25px;line-height:1.6;\"><span style=\"font-size:12pt;white-space:pre-wrap;\">Strong documentation, communication, and presentation skills.</span></li><li style=\"font-size:12pt;margin:3px 0px;letter-spacing:0.25px;line-height:1.6;\"><span style=\"font-size:12pt;white-space:pre-wrap;\">US Citizen.</span></li></ul><p style=\"font-family:&quot;Basel Grotesk&quot;,Arial,sans-serif;font-size:6pt;font-weight:400;line-height:1.6;letter-spacing:0.25px;margin:4px 0px;padding:0px;\"><b><strong style=\"font-size:13pt;white-space:pre-wrap;\">Roles and Responsibilities</strong></b></p><ul data-pattern=\"discCircleSquare\" data-depth=\"1\" style=\"font-family:&quot;Basel Grotesk&quot;,Arial,sans-serif;font-size:11pt;font-weight:400;margin:8px 0px;line-height:1.6;padding:0px 0px 0px 32px;list-style-type:disc;\"><li style=\"font-size:12pt;margin:3px 0px;letter-spacing:0.25px;line-height:1.6;\"><span style=\"font-size:12pt;white-space:pre-wrap;\">Ability to learn and use HyperX for preliminary and detail analysis/design sizing optimization of full airframe and space vehicles. 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Document design and analyses results.</span></li><li style=\"font-size:12pt;margin:3px 0px;letter-spacing:0.25px;line-height:1.6;\"><span style=\"font-size:12pt;white-space:pre-wrap;\">Candidates will be reporting directly to NASA and industry OEM customers and must be able to verify and describe the application of external loadings and their resolution into critical internal mechanical and thermal load paths, and to the resulting optimum design and their margins of safety.</span></li><li style=\"font-size:12pt;margin:3px 0px;letter-spacing:0.25px;line-height:1.6;\"><span style=\"font-size:12pt;white-space:pre-wrap;\">Ensure project issues are resolved in a timely fashion with your related experience and competence and an ability to create workaround procedures when needed. Escalate urgent problems requiring more in-depth knowledge to appropriate engineering leads.</span></li><li style=\"font-size:12pt;margin:3px 0px;letter-spacing:0.25px;line-height:1.6;\"><span style=\"font-size:12pt;white-space:pre-wrap;\">Participate in overall HyperX software testing and provide your suggestions to development and modification of the software.</span></li></ul><p style=\"font-family:&quot;Basel Grotesk&quot;,Arial,sans-serif;font-size:6pt;font-weight:400;line-height:1.6;letter-spacing:0.25px;margin:4px 0px;padding:0px;\"><b><strong style=\"font-size:13pt;white-space:pre-wrap;\">Benefits</strong></b></p><ul data-pattern=\"discCircleSquare\" data-depth=\"1\" style=\"font-family:&quot;Basel Grotesk&quot;,Arial,sans-serif;font-size:11pt;font-weight:400;margin:8px 0px;line-height:1.6;padding:0px 0px 0px 32px;list-style-type:disc;\"><li style=\"font-size:12pt;margin:3px 0px;letter-spacing:0.25px;line-height:1.6;\"><span style=\"font-size:12pt;white-space:pre-wrap;\">Competitive salary and benefits (PTO, 401(k), health insurance, HSA/HRA eligibility, life and disability insurances)  </span></li><li style=\"font-size:12pt;margin:3px 0px;letter-spacing:0.25px;line-height:1.6;\"><span style=\"font-size:12pt;white-space:pre-wrap;\">Exposure and involvement with many companies and their current aircraft designs (commercial transports/UAM eVTOLS/military planes) and space launch designs (commercial rockets/space tourism vehicles/demonstrator X planes)</span></li><li style=\"font-size:12pt;margin:3px 0px;letter-spacing:0.25px;line-height:1.6;\"><span style=\"font-size:12pt;white-space:pre-wrap;\">Occasional travel to customer facilities</span></li><li style=\"font-size:12pt;margin:3px 0px;letter-spacing:0.25px;line-height:1.6;\"><span style=\"font-size:12pt;white-space:pre-wrap;\">Small company, large impact</span></li><li style=\"font-size:12pt;margin:3px 0px;letter-spacing:0.25px;line-height:1.6;\"><span style=\"font-size:12pt;white-space:pre-wrap;\">Passionate coworkers</span></li><li style=\"font-size:12pt;margin:3px 0px;letter-spacing:0.25px;line-height:1.6;\"><span style=\"font-size:12pt;white-space:pre-wrap;\">Company events and conferences</span></li></ul>",
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    "applicationConfirmationTemplate": "67d05dc3fd0ea0b9c95a3c65",
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  "detail_meta": {
    "url": "https://ats.rippling.com/api/v2/board/collieraerospace/jobs/f2dd7c17-0959-4ce4-85ba-b614a5b0ae74",
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}
Get this page with API

Rendered from the bluedoor Job Postings API. Reproduce it:

GET https://api.bluedoor.sh/job-postings/v1/jobs/67cb66e5dda1a5abf2433f56b9aa6366302fe526?include=descriptionJSON
GET https://api.bluedoor.sh/job-postings/v1/orgs/9f91f6c2-86ba-422d-b262-81658ea68dc3JSON
GET https://api.bluedoor.sh/job-postings/v1/sources/4c4042bb-39e7-4fd9-9845-078a573780cdJSON
GET https://api.bluedoor.sh/job-postings/v1/jobs/67cb66e5dda1a5abf2433f56b9aa6366302fe526/eventsJSON