Engineer Rotordynamics for Rockets Based at Hebbal

Engineer Rotordynamics for Rockets Based at Hebbal

1 Nos.
154707
Full Time
3.0 Year(s) To 10.0 Year(s)
30.00 LPA TO 35.00 LPA
Job Description:
 
2. Rotordynamics
 
You will be responsible for rotordynamic analysis and mechanical design of high-speed rotating machinery for rocket turbopump applications, including rotor dynamics, vibration, bearing and seal interactions, and stability assessment.
 
KEY RESPONSIBILITIES
 
•    Owning the rotordynamics of the turbopumps, including shaft, bearing and seal characteristics, stiffness and damping.
•    Analyzing critical speeds, mode shapes, Campbell diagrams and stability of the turbopumps.
•    Supporting cold-flow and hot testing of turbopumps: executing tests, analyzing vibration data, mapping critical speeds and studying the stability of the system.
•    Supporting modal analysis and vibration testing, and correlating analytical results with experimental data.
•    Collaborating with the turbomachinery design, mechanical design and test engineering teams.
•    Presenting the rotordynamic analysis, test plans and test results at the PDR, TDR and VDR, closing out review actions and getting clearance at each stage.
 
REQUIRED QUALIFICATION
 
•    Strong fundamentals in rotordynamics, mechanical vibrations and structural dynamics.
•    Understanding of bearings, seals, shaft design and rotor-support systems.
•    Knowledge of Campbell diagrams, critical speeds, mode shapes and stability analysis.
•    Understanding of rotor balancing, unbalance response, vibration and instability mechanisms.
•    Familiarity with ANSYS Rotordynamics or equivalent.
•    Proficiency in Python for engineering calculations and data analysis.
 
PREFERRED QUALIFICATION
 
•    Academic projects, internships or industry experience in rotordynamics, turbomachinery or high-speed rotating equipment.
•    Exposure to modal testing, vibration instrumentation and experimental validation.
 
 
Key Skills :
Company Profile

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