Senior Thermofluids Analyst - Electron

Rocket Lab is a vertically integrated provider of small launch services, satellites, and spacecraft components. Our mission is to open access to space to improve life on Earth. Our team is over 1,500 people strong and we're adding to it every week. Collaboration is at our core – every idea is heard, and everyone makes a difference. Teams are nimble, decisions are made quickly, and we are action oriented.While other companies talk about it, we do it!About the roleRocket Lab's analysis team contributes to the operation and development of Electron by using modelling and simulation to solve challenging problems involving dynamics, fluid flow, and thermodynamics. You will be the technical owner of propellant, pressure-loss and gas budgets and systems across the Electron launch Vehicle. Whether it is using CFD to predict the heating on the vehicle during ascent, 1D flow of propellants and gasses, or data analysis to demonstrate vehicle performance, analysis is critical to the operation and development of a robust launch vehicle.As a Thermofluids Analyst in Rocket Lab's Analysis team you will contribute to the analysis, design validation, and future improvements of Rocket Lab's Electron launch vehicle, Space Systems, and Space Components. Day to day, you will be expected to analyse flight data, define loads and environments, perform detailed simulations and physics-based analysis, guide design, and help validate analysis, design, and system performance through test. Scope of work may additionally extend to supporting launch and test ground systems, propulsion development, launch operations, and customer interaction.Key DutiesPerform, validate, and document CFD analyses of launch vehicle fluid systems including: Compressible flow (choked flow, Aerodynamics)Incompressible flow (internal, two phase)Perform heat transfer simulations (conduction, convection and radiation) including: Conduct integrated thermal analyses (ITAs) of spacecraft integrated to the Electron launch vehicle.Component thermal analysesAeroheating thermal responseTPS specificationPerform, validate, and document thermofluid analyses of primary and secondary launch vehicle systems, including: Model development and codingNumerical AnalysisMaterial selectionPerformance trade-off studiesPerformance optimizationWork closely with design and test engineers to iterate through design concepts, determine test requirements, and demonstrate positive marginsProcess and interpret ground test and flight data, including: Determining if vehicle components remain within MPE boundsComparing sensor data across multiple flights to detect out-of-family resultsIdentifying and resolving sensor configuration issues (grounding, calibration, damage, naming etc.)Using a strong understanding of physical principles (e.g., heat transfer, flow, cryogenics, pumps, etc.) to determine the root cause of vehicle anomalies through data analysisConduct peer reviews of analysesDocument data processing methodology thoroughly for peer review and sign-offProduce Acceptance, Proto-qualification, and Qualification test levels through the consistent application of approved margining approachesSupport testing of vehicle subsystems through correlation of test and analysis results, and preparation of pre and post-test analysis reportsStandardise and catalogue analysis procedures in line with industry best practiceEnsure pump cavitation marginDevelop new and existing propellant dynamics models around temperature, gas rejection and control strategiesContribute to the improvement and automation of test and flight data reviewEssential skillsA degree in Mechanical, Aerospace Engineering or similar field5+ years industry experience, ideally from the Aerospace, Automotive or Marine industriesStrong understanding of physical principles (heat transfer, electronics, internal flow, aerodynamics, etc.)Fluid engineering experience around pressure loss, valves and sensorsDemonstrated experience with one or more industry standard CFD packages: Fluent, CFX, STAR-CCM+Experience in Python and associated scientific packages: numpy, pandas, scipy, matplotlibDemonstrated thermal modelling of components, networks and lump massesExperience with experimental test methods, sensor selection and data post-processing / interpretation (thermocouples, pressure transducers, accelerometers, strain gauges, microphones etc.)The ability to work to deadlines within a high-pressure environmentDesired SkillsExperience with dynamic thermofluid systems: Propellant Dynamics ( slosh, flow instabilities, Pogo )Propellant level sensing and control strategiesPumps, pressurisation systems and cryogenics experienceThermodynamics of 2-phase, cryogenics or refrigeration systemsCompressible gas modelling of pressure vessels, pressurisation systems and pipingKnowledge around space thermal environments and modelling for both orbital and ascent environmentsThermal protection system design, specification and implementation.Knowledge of HVAC system design and/or analysis.Experience with one or more industry standard thermal modelling packages: Thermal Desktop, THERMICA, NX SSTFamiliarity using Solidworks CAD and PDM packages (or comparable industry standard packages) with emphasis on model interrogation and defeaturing for subsequent analysesExperience in Python package development and modelling (git, CI, deployment)Familiarity with industry standards (e.g., MIL-STD-1540, GSFC-STD-7000, ECSS-E-HB-32, NASA-STD-5001)Rocket Lab Employee BenefitsThe opportunity to work on innovative and groundbreaking technologyAn employee stock purchase programAccess to world leading experts to develop your careerUnlimited barista coffee, fruit, and snacksDiscounted health insurance with Southern CrossAdditional parental leave entitlementsA vibrant team culture with social activities throughout the yearIf the above sounds like you apply now!FOR CANDIDATES SEEKING TO WORK IN US OFFICES ONLY:To conform to U.S. Government space technology export regulations, including the International Traffic in Arms Regulations (ITAR), Rocket Lab Employees must be a U.S. citizen, lawful U.S. permanent resident (i.e., current Green Card holder), or lawfully admitted into the U.S. as a refugee or granted asylum, or be eligible to obtain the required authorizations from the U.S. Department of State and/or the U.S. Department of Commerce, as applicable. Learn more about ITAR here .Rocket Lab provides equal employment opportunities to all employees and applicants for employment and prohibits discrimination and harassment of any type without regard to race, color, religion, age, sex, national origin, disability status, genetics, protected veteran status, sexual orientation, gender identity or expression, or any other characteristic protected by federal, state or local laws. This policy applies to all terms and conditions of employment at Rocket Lab, including recruiting, hiring, placement, promotion, termination, layoff, recall, transfer, leaves of absence, compensation and training.Applicants requiring a reasonable accommodation for the application/interview process for a job in the United States should contact Giulia Biow at ******. This dedicated resource is intended solely to assist job seekers with disabilities whose disability prevents them from being able to apply/interview. Only messages left for this purpose will be considered. A response to your request may take up to two business days.FOR CANDIDATES SEEKING TO WORK IN NEW ZEALAND OFFICES ONLY:For security reasons background checks will be undertaken prior to any employment offers being made to an applicant. These checks will include nationality checks as it is a requirement of this position that you be eligible to access equipment and data regulated by the United States' International Traffic in Arms Regulations.Under these Regulations, you may be ineligible for this role if you do not hold citizenship of Australia, Japan, New Zealand, Switzerland, the European Union or a country that is part of NATO, or if you hold ineligible dual citizenship or nationality. For more information on these Regulations, click hereITAR Regulations.#J-18808-Ljbffr