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Posted: 10/20/2026Principal Product Definition Engineer – Gas Turbines
Honeywell Aerospace TechnologiesCore Competencies
Role fitCore Competencies
Use this summary to align your resume positioning with the role.
Demonstrates expertise in gas turbine system design and propulsion technologies, with a strong ability to conduct competitive assessments and develop technical proposals. Proven leadership in managing cross-functional teams and delivering optimized system solutions in aerospace engineering projects.
Highest-signal resume keywords
Gas Turbine System ExperiencePropulsion System StudiesTechnical Proposal DevelopmentLeadership in Cross-Functional TeamsBasis of Estimates (BOE) Generation
About the role
Key responsibilities & impact- Engage in Fan, Shaft, APU and other advanced technology concept studies
- Conduct competitive and roadmap assessments
- Provide system engineering support for conceptual propulsion and APU system studies in IPDS Phase 0-2A
- Support turbofan activity for the IPDS Phase 2 HTF-NG concept
- Support APU activities for wide-body, narrow-body and small APU growth applications
- Support proposals to win customer selection
- Develop clear problem statements for technical disciplines and coordinate associated projects
- Conduct architecture trade studies to develop technically optimized system solutions
- Evaluate alternatives through competitive research and modeling
- Assess customer value propositions
- Develop technical proposal offerings
- Plan, estimate and schedule projects
- Prepare and conduct project status presentations for leadership and external customers
- Evaluate new concepts, practices and approaches
- Motivate cross-functional teams and build relationships with team members and customers
- Resolve conflicts tactfully and effectively
- Exceed customer expectations
Requirements
What you’ll need- U.S. Person status as defined by U.S. export control laws: U.S. citizen, U.S. permanent resident, protected status in the U.S. under asylum or refugee status, or ability to obtain an export authorization
- Bachelor's degree in Mechanical or Aerospace Engineering or a related field
- 10+ years of directly related or equivalent gas turbine system or aerospace systems experience
- Prior experience with Propulsion, APU and Shaft configuration/trade studies desired
- Experience generating Basis of Estimates (BOE’s) for government programs desired
- Experience creating proposals and working directly with external customers desired
- Strong understanding of gas turbine engine design and technology and engineering fundamentals
- Knowledge of gas turbine engine competitor products, technologies and industry trends
- Specialization in at least one aspect of gas turbine design/technology
- Strong decision-making capability with limited or ambiguous information
- Experience working in teams; demonstrated leadership attributes preferred
- Ability to identify key factors in complex tradeoffs and assess optimum system solutions
- Mechanical systems-based experience and perspective desirable
Benefits
Comp & perks- Employer-subsidized medical, dental, vision and life insurance
- Short-term and long-term disability coverage
- 401(k) match
- Flexible spending accounts
- Health savings accounts
- Employee assistance program
- Educational assistance
- Parental leave
- 12 paid holidays
- Paid time off for vacation, personal and sick time
ATS Keywords
✓ Tailor your resumeApplicant Tracking System Keywords
Tip: use these terms in your resume and cover letter to boost ATS matches.
Hard Skills
Gas Turbine Engine DesignAPU System StudiesArchitecture Trade StudiesCompetitive ResearchModeling TechniquesProject PlanningEstimation and SchedulingTechnical Problem StatementsSystem Engineering SupportCustomer Value Proposition Assessment
Soft Skills
Decision-Making CapabilityConflict ResolutionTeam MotivationRelationship BuildingEffective Communication
Industry Keywords
Aerospace EngineeringMechanical EngineeringGas Turbine TechnologyAPU ConfigurationCompetitive AssessmentCustomer EngagementEngineering FundamentalsIndustry TrendsConceptual Propulsion StudiesIPDS Phase 0-2A