Principal or Senior Principal Aeronautical Engineer (Landing Gear)

Northrop Grumman•San Diego, CA

98d•$114,000 - $213,400•Onsite

About The Position

Northrop Grumman Aeronautics Systems is looking to add a Principal or Senior Principal Aeronautical Engineer (Landing Gear) to our team in El Segundo, CA or Rancho Bernardo, CA. The selected candidate will be responsible for development, design, and integration of landing gear on an advanced aircraft. Northrop Grumman's 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.

Requirements

Bachelor’s Degree in a relevant STEM (Science, Technology, Engineering, or Mathematics) discipline with 5 years of related experience; OR a Master’s Degree in a relevant STEM discipline with 3 years of related experience; OR a PhD in a relevant STEM discipline with 1 year of related experience (for Principal level).
Bachelor’s Degree in a relevant STEM (Science, Technology, Engineering, or Mathematics) discipline with 8 years of related experience; OR a Master’s Degree in a relevant STEM discipline with 6 years of related experience; OR a PhD in a relevant STEM discipline with 4 years of related experience (for Senior Principal level).
Prior experience with aircraft landing gear systems and landing gear design
Prior experience with 3D Computer Aided Design (CAD) software applications
Familiarity with industry standard software application tools such as Microsoft Office Suite, Adobe Acrobat, etc.
Current, active in-scope U.S. Government Secret security clearance
Ability to obtain and maintain Special Program Access (SAP).
U.S. Citizenship is required for all positions with a government clearance and certain other restricted positions.

Nice To Haves

Master’s Degree in Mechanical or Aerospace Engineering or related discipline
Expert knowledge of landing gear design including: Landing gear placement (both deployed and retracted positions), Landing gear loads and preliminary sizing, Shock struts, Wheel and tire selection, Braking systems, Retraction and locking systems, Landing gear door sequencing mechanisms
Experience with Siemens NX CAD application, including NX Motion module
Familiarity with development of landing gear doors, door actuation and door locks, as well as the development of in-flight door opening mechanisms
Prior experience leading a team of engineers
Prior experience in coordinating with multiple Integrated Product Teams (IPTs) within a dynamic program environment
Experience with suppliers and supplier coordination

Responsibilities

Identify existing and/or conceptual landing gear systems to meet requirements, creating 3D models and layouts, and performing trade studies to analyze the impact of integrating proposed mechanisms systems onto aircraft, as well as identify main driver variables that most significantly impact top level program requirements.
Support advanced aircraft design efforts with landing gear system design, hardware selection, placement, preliminary sizing, and initial integration into different aircraft configurations. Secondary role is to provide mechanisms design support to other aircraft sub-systems, such as drive systems and door uplocks for in-flight door operation.
Develop landing gear system requirements and create the associated system specifications, supplier procurement specifications, and supplier SOWs. This will include, but is not limited to, creating functional architecture and activity diagrams, in collaboration with other sub-system engineering disciplines to understand power, cooling, signal, and structural interfaces for the landing gear system.
Support the supplier management team by being the primary technical interface between NGAS and landing gear supplier subject matter experts.
Participate in internal program, customer, and supplier technical exchange meetings and formal program milestone reviews to provide and/or obtain progress status updates.
Provide technical guidance to, and coordinate with, multiple engineering design teams, including the aircraft configuration team, the structures team, sub-systems team, and supplier management teams supporting the conceptual, preliminary, and detail design and development of the aircraft.