** Candidates should have really strong GD&T (Geometric Dimensioning and Tolerencing) experience. Please provide summaries of candidates GD&T experience on their resumes **
** Candidates must have significant experience with Creo. Windchill experience strongly preferred.
** 10 years minimum of related experience as technical Design Engineer in rocket propulsion hardware or equivalent, and 10 years minimum of related experience as technical Designer using ProE/Creo CAD systems **
** Knowledge in the design of high pressure cryogenic, ambient and high temperature rocket chambers, nozzles, gas generators, igniters, injectors, valves, actuators and other associated rocket engine hardware is preferred **
Design Engineer - Must be able to create or modify designs of liquid rocket propulsion hardware associated to high pressure and high temperature static structures, combustion systems and high pressure valve systems.
-Responsible for designing, developing and testing products including providing project time and cost estimate, product manufacturing and evaluation product for quality safety and cost.
-Applies research to the planning design, development and testing of rocket chambers, nozzles, gas generators, igniters, injectors, valves, actuators and other associated rocket engine hardware.
-Applies theories of heat and energy transfer to create practical solutions to technical problems
-Responsible for damage tolerance, durability, design modeling, coordination with analysis disciplines.
-Majority of work will be to develop and maintain component and assembly layouts, designs/CAD models, and drawings using Creo2 graphics system for liquid engine hardware.
Activities: conceptual design creation, design layouts, GD&T application, tolerance analysis, systems design and integration, fabrication process identification, synthesis of higher level requirements to component level requirements. Conduct trade studies and develop schedules, test plans, component specifications and procedures.