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Hybrid Power & Energy Systems - IPT Head
LTTS Canada Branch
Montreal-Est (CSLS0804), Quebec (CLS0105)
Job Description
Job Title: IPT Lead - Hybrid Power & Energy Systems
Key Responsibilities
Lead the Hybrid Power & Energy Systems IPT and ensure alignment with aircraft program objectives.
Own scope, schedule, cost, quality, and technical delivery.
Coordinate across Propulsion, Electrical Systems, Thermal Management, Flight Controls, and Avionics teams.
Serve as the primary technical interface with customers, suppliers, and stakeholders.
System Architecture & Design
Define hybrid-electric propulsion architectures, including battery systems, electric motors, generators, power electronics, and energy management systems.
Perform system sizing, trade studies, energy flow analysis, and efficiency optimization.
Develop and manage System Requirement Documents (SRD), Interface Control Documents (ICD), and power distribution architectures.
Integration & Systems Engineering
Lead integration of electrical propulsion, power distribution, and thermal management systems.
Ensure compatibility with aircraft electrical networks, flight controls, structural constraints, and avionics systems.
Drive Model-Based Systems Engineering (MBSE) practices throughout development.
Verification, Validation & Testing
Define and execute MIL, HIL, ground, and flight test validation strategies.
Validate system performance, energy efficiency, thermal behavior, reliability, and safety.
Ensure complete requirements traceability from design to validation.
Certification & Compliance
Lead certification activities in accordance with FAA, EASA, and DGCA requirements.
Ensure compliance with ARP4754A, ARP4761, and DO-160 standards.
Support evolving certification requirements for electric and hybrid propulsion systems.
Manage compliance documentation, safety assessments, and test reports.
Safety & Reliability Engineering
Conduct FHA, FMEA, and FTA activities.
Ensure battery safety, thermal runaway mitigation, fault tolerance, redundancy, and robust energy management strategies.
Drive reliability-focused system design and risk mitigation.
Stakeholder Management
Present architecture concepts, performance metrics, and risk mitigation plans to customers and leadership teams.
Support RFQs, proposals, effort estimation, and technology roadmap development.
Risk & Configuration Management
Identify and mitigate electrical, thermal, and integration risks.
Ensure adherence to configuration management and change control processes.
Manage dependencies across IPTs and development teams.
Required Qualifications
Education
Bachelor's or Master's degree in Electrical Engineering, Aerospace Engineering, Energy Systems, or Power Electronics.
Experience
12-18+ years of experience in aerospace, automotive EV, or energy systems domains.
Strong experience in hybrid/electric propulsion systems and advanced mobility programs.
Proven leadership experience managing cross-functional IPT teams.
Technical Skills
Hybrid propulsion architectures and energy storage technologies.
Battery systems, power electronics, and electrical machines.
Energy management, optimization, and thermal management systems.
MATLAB/Simulink, PSCAD, AMESim, and MBSE tools (Cameo, Rhapsody).
Knowledge of ARP4754A, ARP4761, DO-160, high-voltage aerospace systems, and EMI/EMC considerations.
Preferred Skills
Experience in eVTOL, UAV, or Advanced Air Mobility programs.
Exposure to sustainable aviation technologies and hydrogen fuel cells.
Familiarity with PLM tools such as 3DX and Teamcenter.
Reporting Structure
Reports To: Chief Engineer / Program Manager
Leads: Hybrid Power & Energy Systems IPT (Electrical, Battery, Integration, and V&V Engineers)
Key Responsibilities
Lead the Hybrid Power & Energy Systems IPT and ensure alignment with aircraft program objectives.
Own scope, schedule, cost, quality, and technical delivery.
Coordinate across Propulsion, Electrical Systems, Thermal Management, Flight Controls, and Avionics teams.
Serve as the primary technical interface with customers, suppliers, and stakeholders.
System Architecture & Design
Define hybrid-electric propulsion architectures, including battery systems, electric motors, generators, power electronics, and energy management systems.
Perform system sizing, trade studies, energy flow analysis, and efficiency optimization.
Develop and manage System Requirement Documents (SRD), Interface Control Documents (ICD), and power distribution architectures.
Integration & Systems Engineering
Lead integration of electrical propulsion, power distribution, and thermal management systems.
Ensure compatibility with aircraft electrical networks, flight controls, structural constraints, and avionics systems.
Drive Model-Based Systems Engineering (MBSE) practices throughout development.
Verification, Validation & Testing
Define and execute MIL, HIL, ground, and flight test validation strategies.
Validate system performance, energy efficiency, thermal behavior, reliability, and safety.
Ensure complete requirements traceability from design to validation.
Certification & Compliance
Lead certification activities in accordance with FAA, EASA, and DGCA requirements.
Ensure compliance with ARP4754A, ARP4761, and DO-160 standards.
Support evolving certification requirements for electric and hybrid propulsion systems.
Manage compliance documentation, safety assessments, and test reports.
Safety & Reliability Engineering
Conduct FHA, FMEA, and FTA activities.
Ensure battery safety, thermal runaway mitigation, fault tolerance, redundancy, and robust energy management strategies.
Drive reliability-focused system design and risk mitigation.
Stakeholder Management
Present architecture concepts, performance metrics, and risk mitigation plans to customers and leadership teams.
Support RFQs, proposals, effort estimation, and technology roadmap development.
Risk & Configuration Management
Identify and mitigate electrical, thermal, and integration risks.
Ensure adherence to configuration management and change control processes.
Manage dependencies across IPTs and development teams.
Required Qualifications
Education
Bachelor's or Master's degree in Electrical Engineering, Aerospace Engineering, Energy Systems, or Power Electronics.
Experience
12-18+ years of experience in aerospace, automotive EV, or energy systems domains.
Strong experience in hybrid/electric propulsion systems and advanced mobility programs.
Proven leadership experience managing cross-functional IPT teams.
Technical Skills
Hybrid propulsion architectures and energy storage technologies.
Battery systems, power electronics, and electrical machines.
Energy management, optimization, and thermal management systems.
MATLAB/Simulink, PSCAD, AMESim, and MBSE tools (Cameo, Rhapsody).
Knowledge of ARP4754A, ARP4761, DO-160, high-voltage aerospace systems, and EMI/EMC considerations.
Preferred Skills
Experience in eVTOL, UAV, or Advanced Air Mobility programs.
Exposure to sustainable aviation technologies and hydrogen fuel cells.
Familiarity with PLM tools such as 3DX and Teamcenter.
Reporting Structure
Reports To: Chief Engineer / Program Manager
Leads: Hybrid Power & Energy Systems IPT (Electrical, Battery, Integration, and V&V Engineers)
Job Requirement
Job Title: IPT Lead - Hybrid Power & Energy Systems
Key Responsibilities
Lead the Hybrid Power & Energy Systems IPT and ensure alignment with aircraft program objectives.
Own scope, schedule, cost, quality, and technical delivery.
Coordinate across Propulsion, Electrical Systems, Thermal Management, Flight Controls, and Avionics teams.
Serve as the primary technical interface with customers, suppliers, and stakeholders.
System Architecture & Design
Define hybrid-electric propulsion architectures, including battery systems, electric motors, generators, power electronics, and energy management systems.
Perform system sizing, trade studies, energy flow analysis, and efficiency optimization.
Develop and manage System Requirement Documents (SRD), Interface Control Documents (ICD), and power distribution architectures.
Integration & Systems Engineering
Lead integration of electrical propulsion, power distribution, and thermal management systems.
Ensure compatibility with aircraft electrical networks, flight controls, structural constraints, and avionics systems.
Drive Model-Based Systems Engineering (MBSE) practices throughout development.
Verification, Validation & Testing
Define and execute MIL, HIL, ground, and flight test validation strategies.
Validate system performance, energy efficiency, thermal behavior, reliability, and safety.
Ensure complete requirements traceability from design to validation.
Certification & Compliance
Lead certification activities in accordance with FAA, EASA, and DGCA requirements.
Ensure compliance with ARP4754A, ARP4761, and DO-160 standards.
Support evolving certification requirements for electric and hybrid propulsion systems.
Manage compliance documentation, safety assessments, and test reports.
Safety & Reliability Engineering
Conduct FHA, FMEA, and FTA activities.
Ensure battery safety, thermal runaway mitigation, fault tolerance, redundancy, and robust energy management strategies.
Drive reliability-focused system design and risk mitigation.
Stakeholder Management
Present architecture concepts, performance metrics, and risk mitigation plans to customers and leadership teams.
Support RFQs, proposals, effort estimation, and technology roadmap development.
Risk & Configuration Management
Identify and mitigate electrical, thermal, and integration risks.
Ensure adherence to configuration management and change control processes.
Manage dependencies across IPTs and development teams.
Required Qualifications
Education
Bachelor's or Master's degree in Electrical Engineering, Aerospace Engineering, Energy Systems, or Power Electronics.
Experience
12-18+ years of experience in aerospace, automotive EV, or energy systems domains.
Strong experience in hybrid/electric propulsion systems and advanced mobility programs.
Proven leadership experience managing cross-functional IPT teams.
Technical Skills
Hybrid propulsion architectures and energy storage technologies.
Battery systems, power electronics, and electrical machines.
Energy management, optimization, and thermal management systems.
MATLAB/Simulink, PSCAD, AMESim, and MBSE tools (Cameo, Rhapsody).
Knowledge of ARP4754A, ARP4761, DO-160, high-voltage aerospace systems, and EMI/EMC considerations.
Preferred Skills
Experience in eVTOL, UAV, or Advanced Air Mobility programs.
Exposure to sustainable aviation technologies and hydrogen fuel cells.
Familiarity with PLM tools such as 3DX and Teamcenter.
Reporting Structure
Reports To: Chief Engineer / Program Manager
Leads: Hybrid Power & Energy Systems IPT (Electrical, Battery, Integration, and V&V Engineers)
Key Responsibilities
Lead the Hybrid Power & Energy Systems IPT and ensure alignment with aircraft program objectives.
Own scope, schedule, cost, quality, and technical delivery.
Coordinate across Propulsion, Electrical Systems, Thermal Management, Flight Controls, and Avionics teams.
Serve as the primary technical interface with customers, suppliers, and stakeholders.
System Architecture & Design
Define hybrid-electric propulsion architectures, including battery systems, electric motors, generators, power electronics, and energy management systems.
Perform system sizing, trade studies, energy flow analysis, and efficiency optimization.
Develop and manage System Requirement Documents (SRD), Interface Control Documents (ICD), and power distribution architectures.
Integration & Systems Engineering
Lead integration of electrical propulsion, power distribution, and thermal management systems.
Ensure compatibility with aircraft electrical networks, flight controls, structural constraints, and avionics systems.
Drive Model-Based Systems Engineering (MBSE) practices throughout development.
Verification, Validation & Testing
Define and execute MIL, HIL, ground, and flight test validation strategies.
Validate system performance, energy efficiency, thermal behavior, reliability, and safety.
Ensure complete requirements traceability from design to validation.
Certification & Compliance
Lead certification activities in accordance with FAA, EASA, and DGCA requirements.
Ensure compliance with ARP4754A, ARP4761, and DO-160 standards.
Support evolving certification requirements for electric and hybrid propulsion systems.
Manage compliance documentation, safety assessments, and test reports.
Safety & Reliability Engineering
Conduct FHA, FMEA, and FTA activities.
Ensure battery safety, thermal runaway mitigation, fault tolerance, redundancy, and robust energy management strategies.
Drive reliability-focused system design and risk mitigation.
Stakeholder Management
Present architecture concepts, performance metrics, and risk mitigation plans to customers and leadership teams.
Support RFQs, proposals, effort estimation, and technology roadmap development.
Risk & Configuration Management
Identify and mitigate electrical, thermal, and integration risks.
Ensure adherence to configuration management and change control processes.
Manage dependencies across IPTs and development teams.
Required Qualifications
Education
Bachelor's or Master's degree in Electrical Engineering, Aerospace Engineering, Energy Systems, or Power Electronics.
Experience
12-18+ years of experience in aerospace, automotive EV, or energy systems domains.
Strong experience in hybrid/electric propulsion systems and advanced mobility programs.
Proven leadership experience managing cross-functional IPT teams.
Technical Skills
Hybrid propulsion architectures and energy storage technologies.
Battery systems, power electronics, and electrical machines.
Energy management, optimization, and thermal management systems.
MATLAB/Simulink, PSCAD, AMESim, and MBSE tools (Cameo, Rhapsody).
Knowledge of ARP4754A, ARP4761, DO-160, high-voltage aerospace systems, and EMI/EMC considerations.
Preferred Skills
Experience in eVTOL, UAV, or Advanced Air Mobility programs.
Exposure to sustainable aviation technologies and hydrogen fuel cells.
Familiarity with PLM tools such as 3DX and Teamcenter.
Reporting Structure
Reports To: Chief Engineer / Program Manager
Leads: Hybrid Power & Energy Systems IPT (Electrical, Battery, Integration, and V&V Engineers)