Senior Space Vehicle Design and Integration Engineer

Senior Space Vehicle Design and Integration Engineer

Company:

The Boeing Company

Job ID:

00000395023

Date Posted:

2023-12-05

Location:

USA - El Segundo, CA

Job Description Qualifications:

The Boeing Company is seeking a motivated Senior Space Vehicle Design and Integration Engineer in El Segundo, CA.

Our teams are currently hiring for a broad range of experience levels including: Lead & Senior Engineer.

Boeing offers a comprehensive benefits package including generous Paid Time Off (PTO), flexible work environment, paid parental leave, 401k matching, very generous tuition assistance for earning advanced degrees, and paid medical leave programs.  For more information, click here.

Position 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
• 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 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 and continuous improvements
• Investigates emerging technologies to develop concepts for future product designs

This position is expected to be 100% onsite.  The selected candidate will be required to work onsite at one of the listed location options.

This position requires the ability to obtain a U.S. Secret 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.

Basic Qualifications (Required Skills/Experience):

• Bachelor's, degree or higher degree from an accredited course of study in engineering
• 5 or more years of experience in technical or engineering field
• 5 or more years of experience on space, launch vehicle, or satellite programs

Preferred Qualifications (Desired Skills/Experience):

• 10 or more years' related work experience or an equivalent combination of education and experience (level 5)
• Experience with multi-disciplined development in any of the following areas: Space structural and mechanical design; Space System integration and test; Space Systems Engineering Mechanical systems and vehicle design architecture

Typical Education & Experience:

Level 4

Education/experience typically acquired through advanced technical education from an accredited course of study in engineering (e.g. Bachelor) and typically 9 or more years' related work experience or an equivalent combination of technical education and experience (e.g. PhD+4 years' related work experience, Master+7 years' related work experience). In the USA, ABET accreditation is the preferred, although not required, accreditation standard.

Level 5
Education/experience typically acquired through advanced technical education from an accredited course of study in engineering  (e.g. Bachelor) and typically 14 or more years' related work experience or an equivalent combination of technical education and experience (e.g. PhD+9 years' related work experience,