University degree in Mechanical or Aerospace Engineering, or equivalent Relevant experience with the composite part design process including composites stacking sequence, classic laminate theory, joints and manufacturing process Excellent knowledge of and a minimum of 5 years proven experience in FE structural analysis (using NASTRAN, FEMAP / ABAQUS is a plus) on composite aircraft structures as well as experience in deploying classical hand-calculation and stress analysis methods and utilizing Aerospace industry standard reference sources Ability to closely cooperate in a multidisciplinary, vertically-integrated team as well as to work and maintain focus on a wide range of tasks simultaneously Highly motivated individual with the ability to work under challenging timescales in a dynamic and responsive environment as well as willingness to independently handle and take ownership of assigned tasks Fluent in English (C1 verbal and written), German verbal language skills count as an asset