Airframe Stress Engineer at Joby Aviation in Santa Cruz, CA

Summary: Joby Aviation is a pioneering company in urban air mobility, working towards certifying their aircraft with the FAA. They are seeking a passionate stress engineer to play a key role in the design of their aircraft, focusing on structural integrity and analysis of aircraft components. Responsibilities: - Conducting design trades, optimizations for final product configuration definitions considering safety, strength, weight, & producibility - Extraction and utilization of finite element analysis internal loads data - Detailed sizing, static, dynamic, damage tolerance, and modal analysis of major structural aircraft components utilizing both classical hand calculations and finite element analysis - Composite ply stack optimization for weight reduction while maintaining manufacturing constraints - Supporting design reviews and signing off on structural parts - Overseeing and supporting structural tests, including definition, planning, requirements, and report writing - Directly communicating with IPTs, design team, DERs, and integration teams Required Qualifications: - B.S. in aerospace engineering, mechanical engineering, or another relevant discipline - 1-2 years of demonstrated working experience in relevant industry, including internships, co-ops, academic research, or project experience - In-depth understanding of loading scenarios, free body diagrams, and structural behavior of aircraft components - Excellent problem-solving skills - Highly proactive attitude with the ability to manage multiple assignments - Strong written and verbal communication skills - Advanced proficiency in finite element analysis, including nonlinear static and dynamic analysis of composite structures or metallic structures - Ability to generate and review detailed analysis reports and aircraft type certification documents - Proficiency with CAD - Ability to be onsite in Santa Cruz, CA Preferred Qualifications: - B.S./M.S. in relevant discipline - Expert knowledge of Femap/Nastran - Experience performing analysis on aircraft primary structure - Strong understanding of composite laminate theory - Experience with bonded joints - Hands on experience working within aircraft certification program - Good understanding of composite materials and manufacturing processes - Excellent understanding of FAR Part 23 and 27 regulations - Experience with MRB - Experience with Dassault Systems CAD - Experience with SLIM/VISION Required Skills: Finite element analysis, Nonlinear static analysis, Dynamic analysis, Composite structures, Metallic structures, Aircraft structural analysis, Load case development, Aircraft certification documentation, CAD, Femap, Nastran, Composite laminate theory, Bonded joints, Aircraft certification program, Composite materials, Manufacturing processes, FAR Part 23 regulations, FAR Part 27 regulations, MRB, Dassault Systems CAD, SLIM Benefits: Paid time off, Healthcare benefits, A 401(k) plan with a company match, An employee stock purchase plan (ESPP), Short-term and long-term disability coverage, Life insurance, And more.