Development of Blade Stage-1 of LP Compressor for Aero Engine
Indigenous design, development, and manufacture of Stage-1 rotor blades for the Low-Pressure (LP) Compressor in aero engines, ensuring compatibility with existing configurations while delivering high performance, reliability, and material integrity.
Primary Focus Area –Aerospace & Avionics Engineering, Electronics and Communication Engineering
Application Start Date -2025-08-21
Application Last Date -2025-09-05
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Link to know more and apply: https://www.tdf.drdo.gov.in/project