Chief/Fellow Performance Engineer

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If you’re looking for a workplace that thrives on creativity, collaboration, and expertise, you’ve found your home!Located in the stunning setting of Jupiter, Florida, FTT is a growing world-class turbomachinery company with a vibrant team of over 300 engineers and technicians, bringing together more than 4,000 years of combined experience in aerospace (military and commercial), industrial, and space turbomachinery. For 25 years, we’ve been at the forefront of next-generation technologies, specializing in rocket turbopumps, aircraft engines, and high-performance jet engines for cruise missiles and unmanned aerial systems (UAS).At FTT, we offer a comprehensive suite of services including design, aerodynamics, performance, heat transfer, rotor dynamics and bearing design, structural analysis, manufacturing, testing, and field support. Our Turbine Technologies division also provides innovative engineering services, testing, and material solutions for military and commercial engines, space propulsion, and industrial power applications.With additional offices in Derby, UK, and Wildau, Germany, we proudly extend our reputation for engineering excellence to the European marketplace, enhancing our access to cutting-edge manufacturing capabilities and a robust supply chain.Our parent company, Kratos Defense and Security Solutions, empowers us to leverage cross-industry capabilities, delivering innovative and cost-effective solutions that benefit our customers.This role is restricted to U.S. citizenship with ability to obtain/maintain security clearance. FTT will require proof of status prior to employment.General Job SummaryThe Chief/Fellow Performance Engineer is a part-time, remote position. The engineer will provide technical oversight on performance analyses in support of engine development and testing programs. Actively participate in programmatic and test data reviews. Will mentor and oversee technical content of junior engineers.Essential Job FunctionsConceptual design and optimization of turbomachinery performance cycles (air breathing engines, rocket turbopumps, and industrial gas turbines) using NPSS and GatesCycle modeling codes. Close coordination with Integrated Product Teams (IPT) on design limits of components related to turbomachinery performance. Review and supervise feasibility studies and testing on new and modified turbomachinery designs. Documents changes through a formal engineering change notification process. Having wide-ranging experience, uses professional concepts and company objectives to resolve complex issues in creative and effective ways. Exercises judgment in selecting methods, techniques, and evaluation criteria for obtaining results. Networks with key contacts outside own area of expertise. Works on complex issues where analysis of situations or data requires an in-depth evaluation of variable factors. Determines methods and procedures on new assignments and may coordinate activities of other personnel (Team Lead). Other job duties as assigned. Supervisory ResponsibilityMay guide or direct support personnel in the preparation of detailed design, design testing, and prototype fabrication.Required ExperienceProficiency in NPSS or GatesCycle codes required. Proficiency in programming codes (C, C++, Java, Fortran, Matlab) is strongly desired. Proficiency in aerodynamic physics and engineering principals with an understanding of practical design limitations. Experienced in all phases of development: conceptual design, analysis, validation, test, and correlation. Maintain sensitive and confidential information as required by company and government requirements. Must be able to work with customers to define and document requirements, address technical concerns, and provide project status. Communicate and interact effectively with peers, supervisors, and public, including maintaining respect for others, and following company policies. Ability to read, understand, and follow instructions. Ability to work in a fast-paced environment. Ability to maintain knowledge, skills, and abilities as it pertains to your job. Excellent written and verbal communications skills. Education And ExperienceBS/MS/PHD in Mechanical or Aerospace engineering. 25+ years’ experience in turbomachinery aerodynamic design and analysis. Work Environment/Physical RequirementsOffice and/or manufacturing environment. Ability to sit and stand for long periods of time. Ability to perform repetitive motion (keyboarding, mouse, phones, rotating wrist, using tools/equipment). Travel RequirementsYes, if applicable.Keyword: performance, aerodynamics, turbomachinery, gatescycle, npss, turbopump, gas turbineKratos Defense is an Equal Opportunity Employer. All qualified applicants will receive consideration for employment without regard to race, color, religion, sex, sexual orientation, gender identity, national origin, age, pregnancy, genetic information, disability, status as a protected veteran, or any other protected category under applicable federal, state, and local laws.Disability Accessibility AccommodationIf you require an accommodation to navigate or apply to our careers site, please send your request to HRAccessibility@kratosdefense.com or call 858-964-2916. Any inquires not related to requesting an accommodation will be discarded.Pay TransparencyThe company will not discharge or in any other manner discriminate against employees or applicants because they have inquired about, discussed, or disclosed their own pay or the pay of another employee or applicant.Job Applicant Privacy NoticeFor applicants in the EU and California residents, please review our privacy notice.From: Kratos DefenseIf you have questions about this posting, please contact support@lensa.com