Staff Rotor/Hub Structural Analyst (Hybrid)

Archer Aviation
San Jose, California, United StatesPosted 20 February 2026

Job Description

<div class="content-intro"><p><span style="font-weight: 400;">Archer is an aerospace company based in San Jose, California building an all-electric vertical takeoff and landing aircraft with a mission to advance the benefits of sustainable air mobility. We are designing, manufacturing, and operating an all-electric aircraft that can carry four passengers while producing minimal noise.</span></p> <p><span style="font-weight: 400;">Our sights are set high and our problems are hard, and we believe that diversity in the workplace is what makes us smarter, drives better insights, and will ultimately lift us all to success. We are dedicated to cultivating an equitable and inclusive environment that embraces our differences, and supports and celebrates all of our team members.</span></p></div><p class="p1">Archer Aviation is seeking a highly motivated, experienced engineer to join our team in revolutionizing the aviation industry. The candidate will support analysis and testing of the rotor system on a new unmanned vehicle platform, including the rotor head, blades, and control system. This role requires expertise of structures of metallic and composite structures and a deep understanding of rotorcraft dynamic systems. Candidate should have a good understanding of fatigue life predictions with a strong background in finite element methods as well as analytical first principles. The ideal candidate will act as a mentor to other members of the team with less experience and establish best practices to follow for the program.</p> <p class="p3"><strong>Responsibilities:</strong></p> <ul class="ul1"> <li class="li1">Perform detailed structural analyses of dynamic system components, including the rotor system, control system, and blades</li> <li class="li1">Evaluate static strength and fatigue life of critical structures using classical hand calculations and finite element analysis for both flight loads and ground load conditions</li> <li class="li1">Evaluate component life and dynamic response of dynamically loaded metallic and composite components subject to high and low cycle fatigue</li> <li class="li1">Author structural substantiation reports and other required technical documentation to meet program needs</li> <li class="li1">Support full scale component ground testing and flight testing, including test requirements, layout, instrumentation, and data reduction</li> <li class="li4">Develop best practices for structural analysis of critical aerospace structures</li> <li class="li1">Collaborate with the aerodynamics and loads dynamics teams to design high performance propeller and rotor blades<span class="Apple-converted-space"> </span></li> <li class="li4">Collaborate with internal and external customers to ensure on-time delivery of data</li> </ul> <p class="p1"><span class="s2"><strong>Qualifications:</strong></span></p> <ul class="ul1"> <li class="li1"><span class="s2">Bachelor’s degree in aerospace engineering, mechanical engineering, or related field</span></li> <li class="li1"><span class="s2">5+ years of experience in design and analysis of critical aircraft structures</span></li> <li class="li1"><span class="s2">Proficient in ANSYS, NASTRAN, or other FE software</span></li> <li class="li7">Knowledge of fatigue and damage tolerance of composites</li> <li class="li7">Knowledge of high cycle and low cycle fatigue in metallic components</li> <li class="li1"><span class="s2">Ability to read engineering drawings and interpret CAD models</span></li> <li class="li1"><span class="s2">CAD design experience (NX preferred)</span></li> <li class="li1"><span class="s2">Strong technical, written, and verbal communication skills</span></li> <li class="li1"><span class="s2">Experience in a fast-paced design environment</span></li> </ul> <p><strong><span class="s2">Preferred:</span></strong></p> <ul class="ul1"> <li class="li1"><span class="s2">Master’s in aerospace engineering, mechanical engineering, or related field</span></li> <li class="li1" ... (truncated, view full listing at source)