Structural & Payload Design Engineer (Senior or Principal)

Boeing•El Segundo, CA

5d•Onsite

About The Position

Boeing Defense, Space & Security (BDS) is seeking a Senior or Principal Structural & Payload Design Engineer (Level 5 or 6) in El Segundo, CA. At Boeing, we are all innovators on a mission to connect, protect, explore and inspire. From the seabed to outer space, you’ll learn and grow, doing work that shapes the world. Find your future with us.

Requirements

Bachelor of Science degree in Engineering (with a focus in Electrical, Mechanical or Aeronautical), Computer Science, Data Science, Mathematics, Physics, Chemistry or non-US equivalent qualifications directly related to the work statement
10+ years of experience in spacecraft/satellite system design, development, test and evaluation
Must meet U.S. export control compliance requirements. To meet U.S. export control compliance requirements, a “U.S. Person” as defined by 22 C.F.R. §120.62 is required. “U.S. Person” includes U.S. Citizen, U.S. National, lawful permanent resident, refugee, or asylee.
Ability to obtain a U.S. Security Clearance for which the U.S. Government requires U.S. Citizenship. An interim and/or final U.S. Secret Clearance Post-Start is required.

Nice To Haves

Experience with multi-disciplined development in any of the following areas: Space structural and mechanical design and engineering; System integration and integrated system test; Systems Engineering Mechanical systems and vehicle design architecture

Responsibilities

Manage and directs the Structural and Mechanical Space Vehicle Engineering Design teams including Structures, Analysis, Thermal, Dynamics, Mechanical, Propulsion, Solar Array, Mass Properties, and Blankets from requirements, design, verification, and production support as the Space Vehicle Design Integration Leader
Develops Common Non-Recurring Product Definition (C-NRPD) plans and ensures execution of requirements, design layouts, analysis, testing, and assembly integration in a timely manner to support program milestones
Leads and participates in system level trades to ensure the vehicle design meets all physical, mechanical and environmental requirements while accommodating the required payload, power, propulsion, thermal, communications and attitude control system requirements
Defines structural, mechanical, environmental design and integration requirements and its constituent assemblies and components including both flight and non-flight (GSE) hardware
Leads design and manufacturing integration requirements using DFMAT principles
Leads the layout reviews and program level General Arrangement meetings for collaborative engineering across various disciplines; resolves design integration issues between segment IPTs
Approves Interface Control Drawings/Models including Moving Mechanical Assemblies (MMAs)
Oversee Critical Clearance Control Plan (CCCP) including definition and verification of Critical Clearance Control List activities (CCCL)
Supports and approves manufacturing integration plans, overseeing Digital Mock-Up (DMU) and Virtual Manufacturing (VM) simulation reviews
Leads the development of structural qualification and acceptance test plans
Supports Program milestone reviews (SRR, PDR, CDR, IDR etc.) and Gate Closure/Lien Closures
Supports design non-conformances and resolution during production
Provides program observed lessons learned to aid in continuous improvement
Investigates emerging technologies to develop concepts for future product designs