Launch Vehicle Electrical Engineer

Northrop Grumman; Chandler (AZ); On-site; USD 66,000 - 119,000; Full time

Benefits offered by this job

Relocation assistance

Job summary

Northrop Grumman Space Systems is searching for an Electrical Engineer to be part of our Integration and Test team in Launch Vehicles, at our Chandler, AZ facility. This position will be 100% on-site in Chandler.

The candidate will serve as an Integration and Test Electrical Engineer for one of our launch vehicle programs, requiring the candidate to function in a dynamic multi-disciplinary environment. Daily responsibilities may require direct contact with launch vehicle flight hardware and

Qualifications

• Be completing or has completed their degree (Bachelor’s) from an accredited institution.
• Be majoring in or having majored in an Electrical Engineering or related discipline.
• Be able to obtain a U.S. Government security clearance (U.S. citizenship is a pre-requisite)

Responsibilities

• Performing hands-on electrical testing at a systems level.
• Developing/maintaining procedures for the assembly and test of launch vehicle systems.
• Incorporating hardware and/or software design changes.
• Documenting & dispositioning hardware discrepancies, pursuing root cause & corrective actions
• Some planning and scheduling of day-to-day tasks
• Constant and timely communication with other team members

Skills

Electrical Engineering

Team communication

Problem solving

Multi-tasking

Security clearance

Education

Bachelor's degree in Electrical Engineering

Master's degree in Electrical Engineering

Tools

MES

Job description

Northrop Grumman Space Systems is searching for an Electrical Engineer to be part of our Integration and Test team in Launch Vehicles, at our Chandler, AZ facility. This position will be 100% on-site in Chandler.

The candidate will serve as an Integration and Test Electrical Engineer for one of our launch vehicle programs, requiring the candidate to function in a dynamic multi-disciplinary environment. Daily responsibilities may require direct contact with launch vehicle flight hardware and