Requirement Detail

Job Title Gas Turbine Performance Sr Advanced Engineer
Job Code 210534
Date Posted 09/24/2026
Number Of Positions Available 1
Client Id 20005
Location Phoenix, AZ USA
Pay Rate $58.65/Hour
Job Description
Must have skills:

• Aerospace gas turbine engine steady state Performance and/or transient Operability modeling expertise and experience.  
• I’m not interested in candidates who provided input to or used the output of the analysis done by the Performance or Operability engineers.  
• I need someone who performed the thermodynamic modeling and analysis as a Performance or Operability Engineer.
• Skilled and experienced with building, debugging, and refining NPSS engine cycle models.
• Adept at requirements decomposition
• Work collaboratively and effectively across multiple engineering disciplines to build accurate systems models.
• Operate in a Model Based Systems Engineering environment.
• Work location: Onsite (hybrid 3+ days/wk) is preferred, we but can accommodate remote work.  
• In situations of 100% remote, there may be situations when the person would need to come to the site for a customer critical design reviews or test support.

Gas Turbine Performance Sr Advanced Engineer

Summary:

• This is an outstanding opportunity for an Engineer with aerospace gas turbine engine experience to join the Performance & Operability team. 
• Our gas turbine engines power a wide range of commercial and military aerospace platforms. 
• This position requires the individual to have expertise in steady state and transient thermodynamic cycles and to be highly capable of building, debugging, refining, and maintaining NPSS system thermal models. 
• Effective knowledge transfer of NPSS modeling techniques is an important aspect of this role.  
• Aerospace operates in a Model Based Systems Environment (MBSE) and experience connecting NPSS models to MBSE tools such as Cameo is desired. 
• The Engineer is responsible for engine definition through all phases of the new product introduction (NPI) processes.


Responsibilities:

• Build, debug, refine, and maintain steady state and transient thermal models using NPSS (Numerical Propulsion System Simulation)
• Develop NPSS customer models
• Foster productive knowledge transfer of NPSS modeling techniques
• Perform requirements analysis & requirements decomposition
• Provide test coverage & data reduction to support engine development and qualification
• Communicate effectively to leadership, customers, and peers including presentations and technical reports.
• Work collaboratively across cross-functional disciplines and teams.
 

Desired Characteristics:

• Strong understanding of gas turbine engine steady state and transient thermodynamics and physics
• Skilled and experienced with building, debugging, and refining NPSS engine cycle models.
• Productive mentoring skills that result in technical growth, particularly with NPSS modeling.  
• Experience in MBSE environments and connecting NPSS models to MBSE tools such as Cameo
• Professional verbal & written communication skills; adept in presenting to upper leadership and customers
• Ability to collaborate seamlessly with diverse and global teams
• Self-motivated, able to work with little supervision and take the initiative to get things done
• Adapt quickly and effectively to changing priorities and program needs.
• Manage a variety of complicated tasks simultaneously
• Proven track record of solving complex engineering problems

Required Qualifications:

• Bachelor’s degree from an accredited institution in a technical discipline such as the sciences, technology, engineering
• 4 years of experience with turbine engine Performance & Operability Modeling and Analysis
• Applicants must be a U.S Citizen