Fluid Subsystems Engineer or Principal Fluid Subsystems Engineer
Northrop GrummanAbout the role
Description
At Northrop Grumman, our employees have incredible opportunities to work on revolutionary systems that impact people's lives around the world today, and for generations to come. Our pioneering and inventive spirit has enabled us to be at the forefront of many technological advancements in our nation's history - from the first flight across the Atlantic Ocean, to stealth bombers, to landing on the moon. We look for people who have bold new ideas, courage and a pioneering spirit to join forces to invent the future, and have fun along the way. Our culture thrives on intellectual curiosity, cognitive diversity and bringing your whole self to work — and we have an insatiable drive to do what others think is impossible. Our employees are not only part of history, they're making history.This position is currently contingent on program funding. Start dates are determined after funding confirmation.
Please note: Only external candidates and NG employees who are not currently in AS Engineering will be considered under this requisition.
Northrop Grumman Aeronautics Systems has an opening for a Fluid Subsystems Engineer or Principal Fluid Subsystems Engineer with experience in the design of fluidic subsystems to join our team of qualified, diverse individuals. This role will be located in Melbourne, FL.
In this role, you will be responsible for developing, modifying, and maintaining aircraft subsystems configurations using current engineering design practices and standards. These subsystems include, but are not limited to, Environmental Control Systems (ECS), Liquid Cooling Systems (LCS), Fuel Systems, and Hydraulic Systems.
Responsibilities and duties:
Design tubes/ducts and routing of transport elements related to Environmental Control Systems (ECS), Liquid Cooling Systems (LCS), Fuel Systems, and Hydraulic Systems
Design secondary structural elements (i.e., bracketry) to attach fluidic systems components to aircraft primary structure
Perform design related tasks utilizing the NX and Teamcenter tool suite
Integrate subsystems components into various aircraft applications
Coordinate and collaborate with relevant stakeholder to ensure robust and maintainable configurations are produced
Apply GD&T requirements to models to ensure producibility and manufacturability of designs
Evaluate and verify requirements to ensure airworthiness criteria are met
Attend internal program, customer and/or supplier technical exchange meetings and/or formal program milestone reviews to provide and/or obtain progress status updates
The successful candidate will be a self-starter, well-organized with good problem-solving skills, able to perform effectively despite concurrent work tasks and will possess strong communication, leadership, team coordination and mentoring skills. The successful candidate will also thrive in an aircraft development design environment and be able to react and quickly adapt to changes in aircraft configuration.
This role may be filled as a Fluid Subsystems Engineer or Principal Fluid Subsystems Engineer based on the qualifications outlined below.
Basic Qualifications:
Fluid Subsystems Engineer- Bachelor’s Degree in STEM (Science, Technology, Engineering or Mathematics) discipline from an accredited university and 2 years of engineering experience
Principal Fluid Subsystems Engineer - Bachelor’s Degree in STEM (Science, Technology, Engineering or Mathematics) discipline from an accredited university and 5 years of engineering experience OR Master’s Degree in STEM (Science, Technology, Engineering or Mathematics) and 3 years of engineering experience
Prior experience with aircraft subsystems fluidic routing design and integration
Prior experience with 3D Computer Aided Design (CAD) software applications
Your ability to obtain and/or transfer and maintain the final adjudicated government Secret clearance, and any program access(es) required for the position within a reasonable period of time, as determined by the company
Preferred Qualifications:
Master’s Degree in Mechanical or Aerospace Engineering or related discipline
Experience with the design, specification, selection, and qualification of aircraft fluidic system components (e.g., fittings, valves, etc.)
Aircraft transport element sizing and architecture development experience, including fluid
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