Analyzes, researches and develops structural engineering specifications involving metals, non-metallic or composite structural materials for product design, or operation of product to include structures, mechanical, hydraulic, electrical and electronics, power plant, armament, heating and ventilating, equipment and maintenance designs. Analyzes damage tolerance, durability, design allowables and structural modeling. Specific structural engineering specialties may include dynamics and loads, stability and stress fatigue and thermal analysis. Tools utilized may include CATIA, IDEAS, ProEngineer and a variety of software applications.
Successful candidate will be a member of the F-35 Center Fuselage IPT, supporting the assembly of the Center Fuselage at Palmdale Aircraft Integration Center. Candidate should be experienced in structural analysis methods, including large scale NASTRAN modelling and analysis of metallic and advanced composite structures. Desired skills include familiarity with detailed structural analysis procedures, FEM analysis, PATRAN, layout sizing, structural integrity evaluations, durability and damage tolerance (DaDT) of aircraft structures, material allowables development, acoustic/dynamic evaluations, and weight control. Responsible for liaison support as well as analysis of parts and installation of these parts in the JSF Center Fuselage. Experience should include the development and first-hand assembly line support of aircraft structural parts and assemblies utilizing metallic/composite material (launch vehicle experience considered)
9 Years with Bachelors in Science; 7 Years with Masters; 4 Years with PhD.
Composites, DaDT(Metallics), and MRB support.
Fighter Aircraft experience preferred.
1275 N MANASSERO ST
ANAHEIM, CA 92807