Northrop Grumman Space designs, builds and delivers space, defense and aviation-related systems to customers around the world. Our main products include launch vehicles and related propulsion systems; missile products, subsystems and defense electronics; precision weapons, armament systems and ammunition; satellites and associated space components and services; and advanced aerospace structures.
We are currently seeking an experienced Staff Structural Engineer (Subject Matter Expert for Nozzle Flexseals) to provide leadership to our Nozzle Design and Analysis team in our Promontory offices.
Role description & Responsibilities:
The Nozzle Staff Structural Engineer is responsible to oversee and guide the designing, analyzing, testing and manufacturing of solid rocket motor flexseals for a variety of government and commercial programs. This individual will use their engineering knowledge and creativity to ensure the following:
Consistency in existing design and analysis methodologies.
Technical rigor in supporting new decisions and changes.
Innovative improvements that meet technical, cost, and schedule requirements.
Job Duties:
Ensure all flexseal design and analysis activities meet internal engineering standards and program requirements (technical, cost, schedule)
Review and perform structural analyses of nozzle flexseals.
Provide technical guidance and mentoring to engineering teams in the design, analysis, test, and production of flexseals.
Be the focal point of communication with production teams (including technicians, process engineers, quality, safety and VSETs).
Review updates to drawings and specifications for flexseals.
Conduct and lead trade studies.
Review reports and presentations for design reviews to be given to internal and external customers.
Lead investigations to resolve anomalous or discrepant flexseal behavior.
Lead research and development efforts to improve flexseal designs.
Experience Requirements:
Minimum Experience: 12 years with BS degree in Mechanical or Aerospace Engineering or 10 years with MS degree in Mechanical or Aerospace Engineering; or 8 years with a PhD.
Ability to travel: Travel expectation of 10%
At least 5 years of direct experience in the design and analysis of nozzles for solid rocket motors
Experience Preferred:
Software proficiency in NX, Abaqus, Team Center, EPLM
3D modeling, mechanical drawings, and GD&T
Understanding of manufacturing and inspection processes
Design and analysis experience with bolted joints, metallic and composite structures, and bonded assemblies
Experience training and coaching less experienced engineers
Skills & Qualifications:
Broad understanding of mechanical design, structural analysis, material behavior, testing methods and manufacturing processes related to flexseals.
Excellent written and oral communication skills
Excellent time management and organizational skills
Detail oriented but able to understand the big picture
Education/Certifications
·B.S. degree in Mechanical or Aerospace Engineering