Rocket Turbine Aerodynamics Engineer

Shape efficient rocket turbine gas paths at Astrobase Space Technologies using meanline methods, performance prediction, and turbine aerodynamics. The work is mainly office-based.This Turbine Design Engineer develops components that deliver turbopump power during hot-gas operation. You will analyze impulse, reaction, and partial-admission stages while maintaining performance maps across operating ranges. The position also supports CFD and FEA inputs for gas paths, blades, disks, thermal loads, and vibration.Key Responsibilities:
Develop turbine inlet manifolds, nozzles, blades, and exhaustsPredict performance for impulse and reaction stagesMatch pump and turbine power across operating rangesDefine hot-gas seals and turbine tip clearancesPresent designs through PDR, TDR, and VDRRequirements:
B.E./B.Tech or M.E./M.Tech qualificationTwo to five years in turbine designFundamentals of compressible flow and turbine aerodynamicsCFD and FEA understanding for turbine componentsPython or MATLAB analysis capabilityBring turbine aerodynamics, meanline design, and turbopump power-matching skills to Astrobase’s liquid rocket engines.
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