CSIR-National Aerospace Laboratories (CSIR-NAL), Bangalore
CSIR-National Aerospace Laboratories (CSIR-NAL), Bangalore
Objective: 1) Thermodynamic cycle analysis for 50 N Micro Gas turbine engine (MGT) 2) Development of configuration of 50 N MGT 3) Design and analysis of Compressor, Combustor, Turbine, Nozzle, shaft and axillary systems 4) Development of fabrication drawings 5) Material selection and fabrication of all the engine components 6) Assembly of MGT 7) Design and development of test rig for MGT 8) Performance testing of MGT on the test bed and delivery of engine for flight test
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