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L3Harris Technologies · 2 months ago

Scientist, Systems Integration/Test Engineer ROC

Rochester, NY

Full-time

Onsite

Senior Level, Lead/Staff

$124K/yr - $231K/yr

10+ years exp

L3Harris Technologies is the Trusted Disruptor in the defense industry, dedicated to delivering end-to-end technology solutions. The Chief Integration & Test Engineer will oversee system verification and test planning for spacecraft integration, leading a team through the product life cycle and ensuring successful testing and validation.

CommercialInformation TechnologyNational Security

No H1B

Security Clearance Required

U.S. Citizen Only

Responsibilities

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

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)

Qualification

System integrationSpace vehicle testingRequirements verificationTechnical leadershipSpace hardware integrationFlat SatsSimulatorsRisk managementCustomer interfacingTeam playerCollaboration

Required

Bachelor's Degree and a minimum of 12 years of engineering experience. Graduate Degree and a minimum of 10 years of engineering experience. In lieu of a degree, a minimum of 16 years of engineering experience

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 or Top Secret Clearance

Preferred

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

Team player, capable of working in a fast-paced program environment