Scientist, Integration and Test Engineering

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L3Harris Technologies is the Trusted Disruptor for the global aerospace and defense industry. With customers mission-critical needs always in mind our more than 50000 employees deliver end-to-end technology solutions connecting the space air land sea and cyber domains.

Job Title: Scientist Integration and Test Engineering (CITE)

Job Code: 33805

Job Location:Palm Bay FL

Job Schedule: 9/80 (Every other Friday off)

Job Description:

The Chief Integration & Test Engineer (CITE) will oversee system verification and test planning for the integration of the spacecraft bus mission payload and communication payload culminating in end-to-end testing. Responsibilities include leading a team of I&T engineers through the product life cycle from initial requirement analysis for testability to designing and developing test plans and flows. Additionally this role involves defining planning and implementing strategies for test verification validation qualification and acceptance testing.

Essential Functions:

• Provide mastery-level system integration and test engineering expertise to a team.
• Lead space hardware and software integration and verification testing at acceptance proto-flight and qualification levels for all relevant environments (vibration thermal vacuum)
• Develop verification plans test procedures and test flows and lead the execution of test procedures.
• Document test results in reports to ensure system requirements are met.
• Lead requirements verification for components subsystems and systems.
• managing the Test Bed and Simulators used during integration and test activities.
• Identify and resolve technical issues and anomalies during integration and testing collaborating with cross-functional teams to address discrepancies.
• Collaborate with cross-discipline teams (systems mechanical structural thermal power optical RF electrical) in development integration and execution.
• Represent Space Integration & Test engineering during major system level design reviews including System Requirements Review (SRR) Preliminary Design Reviews (PDR) Critical Design Reviews (CDR) and Test Readiness Reviews (TRR) and Pre-Shipment Review (PSR)
  
  

Qualifications:

• Bachelors Degree and a minimum of 12 years of engineering experience. Graduate Degree and a minimum of 10 years of engineering lieu of a degree a minimum of 16 years of engineeringexperience
• Experience with system-level space requirements verification including allocation testability flow down analysis testing and demonstration.
• Experience executing all phases of space vehicle programs (SRR PDR CDR IRR TRR PSR etc.)
• Experience with space hardware/software integration testing and troubleshooting
• Experience with Flat Sats and simulators
• Secret Clearance

Preferred Additional Skills:

• Technical leadership experience in an SI&T role
• Experience designing Mechanical Ground Support Equipment (MGSE) and/or Electrical Ground Support Equipment (EGSE) for large space vehicles.
• Strong understanding in space vehicle subsystem designs: Power Thermal Communications (Optical or RF) Data Management Structures Mechanisms GNC Propulsion Configuration/Packaging Software Fault Management Harness
• Proficiency with Interface Definition Documents (IDDs) and Interface Control Drawings (ICDs)
• Expertise in requirements management traceability and verification using IBM Rational DOORS and MBSE tools (CAMEO)
• Experience directly interfacing with customers (both prime contractors and end customers) to resolve technical issues during the development and sell-off of space hardware.
• Experience in risk management

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Please be aware many of our positions require the ability to obtain a security clearance. Security clearances may only be granted to U.S. addition applicants who accept a conditional offer of employment may be subject to government security investigation(s) and must meet eligibility requirements for access to classified information.

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