Senior Engineer, Airframe Stress Analysis at Otto Aerospace

, , United States -

Full Time

Start Date

Immediate

Expiry Date

21 Jun, 26

Salary

0.0

Posted On

23 Mar, 26

Experience

5 year(s) or above

Remote Job

Yes

Telecommute

Yes

Sponsor Visa

Skills

Stress Analysis, Finite Element Analysis, Durability and Damage Tolerance, Structural Test Plans, Composite Structures, Metallic Structures, Classical Analysis Methods, FEMAP, CATIA V5/V6/3DX, ENOVIA V5/V6/3DX, FAR Part 23 Certification, Stress Notes Authoring, Configuration Development, Critical Thinking, Problem Solving, Teamwork

Industry

Aviation and Aerospace Component Manufacturing

Description

About Otto Aviation OTTO is developing the world’s first fifth-generation business jet, designed for sustainability through the innovative use of advanced super-laminar aerodynamics and high-precision, net-shaped composites. Flight tests of our technology demonstrator validate a dramatic reduction in fuel burn and allow a sizeable improvement in cabin comfort. Otto Aviation is designing world-class aircraft from first principles physics and delivering ground-breaking aircraft and economic performance. Role Overview Otto Aerospace is seeking a Senior Engineer, Airframe Stress Analysis to be a member of our team. The ideal candidate has relevant stress analysis experience and a willingness to learn. Otto Aerospace is seeking engineers, who are comfortable working from first principles, work great in a team atmosphere and get things done. The successful candidate will join the Structural Analysis department. This department employs classical and finite element analysis techniques to substantiate structure to the requirements. Additionally, they issue inspection plans to ensure the structure's continued airworthiness throughout the aircraft's lifetime. They also author governing documents and test documents, and specifications related to the aircraft structure to be consumed in the design, analysis, inspection and repair of Otto aircraft. What You'll Do Perform stress analysis of metallic and composite structural components, assemblies and systems to provide inputs to the design and ensure structural integrity. Author, review and approve analysis documentation. Create and/or utilize Finite Element Models (FEM). Perform Durability and Damage Tolerance (DADT) assessments. Review and approve the engineering definition for release in the product lifecycle system (PLM). Author, review and approve structural test plans and reports. Compare structural test results to analytical models (test vs Finite Element Model). Develop stress analysis tools and methodologies. Support multi-disciplinary configuration development and trade studies. Interface with materials & processes, structural test laboratories, flight test, manufacturing and customers/regulation authorities. Review, guide and support programs for new, supplemental and experimental certification under FAR Part 23 sub part C & D. Mentor junior team members. Who You Are Education B.S. in Mechanical or Aerospace Engineering, or equivalent Experience 5+ years of relevant industry experience (or 2+ with M.S.) Strong verbal and written communication skills Experience with airframe static and fatigue stress analysis for both composite and metallic structures Knowledge of industry standard classical analysis methods Knowledge of Finite Element Analysis methods (FEMAP experience is a plus) Experience authoring stress notes and stress reports Experience supporting disposition of non-conformances Proficiency with CATIA V5/V6/3DX and ENOVIA V5/V6/3DX Knowledge of typical airframe structural design criteria Knowledge of FAR Part 23 certification requirements and processes Interpersonal Skills Strong verbal and written communication skills Active Listening: Practice to gain insight and truly understand all project stakeholders. Critical Thinking: Make prompt, informed and value-based decisions for the project. Organization: Focus on agenda, schedules, frameworks, and methodologies, as well as communicating tasks, updates, progress, and blockers. Problem Solving: Assess issues from different vantage points and formulate the best solution in addressing specific challenges. Self-Motivation: Exude highest level of commitment and motivation to see it through from start to finish. Teamwork and Team Building: Establish a collaborative culture where people with unique personalities and skills happily work together and accountable to shared goal. Strong Business Communication: Use the right language, tone and storytelling techniques when communicating, describing, or explaining issues over email, chat, reports, presentations and other forms and channels of communication. Ability to work with domestic/international supplies/partners effectively Where You'll Be **This will start as a remote position, with travel to the company's temporary headquarters in Ft Worth, TX, then will transition to on-site at our new location in Jacksonville, FL, upon facility readiness (6-12 months). Benefits Otto Aerospace provides a robust benefits package that includes competitive salaries, subsidized medical, dental, and vision coverage, 401(k) opportunities, paid short term disability, voluntary long-term disability, and additional term life, with 15 paid days off, 13-14 paid holidays, and paid sick leave. Depending on seniority and role, some roles qualify for potential bonuses and stock options. Otto Aerospace is an Equal Opportunity Employer We are committed to diversity, equity, and inclusion in every aspect of our hiring process. All applicants will be considered for employment regardless of race, color, religion, sex, sexual orientation, gender identity, national origin, veteran status, or disability. We believe that a diverse team brings fresh perspectives, innovative ideas, and greater success. The more inclusive we are, the stronger we become. Applicants must be legally authorized to work in the U.S. #LI-Remote

Responsibilities

The engineer will perform stress analysis on metallic and composite components to ensure structural integrity, authoring and approving necessary documentation, and creating/utilizing Finite Element Models. They will also conduct Durability and Damage Tolerance assessments and support the review and approval of structural test plans and reports.