Lead Satellite Electrical Power and Harness Systems Engineer

Boeing•El Segundo, CA

3d•$146,200 - $197,800•Onsite

About The Position

The Boeing Company, Space, Intelligence, and Weapon Systems (SIWS) Team is seeking a Lead Satellite Electrical Power and Harness Systems Engineer (Level 4) to join their team in El Segundo, California. This role involves creating next-generation products and services for commercial and proprietary customers, covering all facets of engineering from technology investment and concept development to proposal writing, requirements and design, build, integration, test, and demonstration. The Electrical Power and Harness Systems Engineer will be part of a high-performing team working on high-intensity development projects, with opportunities to engage in both non-recurring and recurring/sustaining efforts for satellite power and harness subsystems, including systems engineering of power system elements and capabilities.

Requirements

Bachelor of Science degree in Engineering, Engineering Technology (including Manufacturing Technology), Computer Science, Data Science, Mathematics, Physics, Chemistry or non-US equivalent qualifications directly related to the work statement
9+ years of related work experience or an equivalent combination of technical education and experience
5+ years of experience working with space related electrical power and harness subsystems
Active U.S. Top Secret/SCI Security Clearance
Must 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.
U.S. Citizenship Required

Nice To Haves

Experience with Satellite Systems Engineering Processes
Experience with Satellite Mission Operations

Responsibilities

Ensure integrated execution and alignment of subsystem with Program EPS/Harness Integrated Product Team Lead
Program execution for EPS/Harness subsystems engineering
EPS/Harness portions of spacecraft and system specifications
System Requirements definition, System flow down and System verification
End-to-End responsibility of EPS/Harness Subsystem through life cycle
Unit Requirements definition, Unit specifications (with REA support)
Subsystem Architecture & Sizing (including Block Diagrams)
Comprehensive specifications, Specification development and maintenance (subsystem and unit specs)
Technology insertion (roadmap)
Unit data buyoff
Inputs to EPS/Harness subsystem-level test procedure development
Facilitate design reviews as required (PDR, CDR, etc.)
Subsystem to Subsystem Interface Requirements
Unit Qualification Support
Inputs to Spacecraft Database, flight software, and flight operating procedures
EPS/Harness Subsystem Launch and Mission Readiness
Participate and Support with cost and schedule reduction initiatives
EPS/Harness Subsystem Mission responsibilities including launch and mission