Propulsion Division

Propulsion Division is mainly involved in applied research in critical areas of gas turbine engine, high speed combustion and development of Wankel rotary engines. The division has contributed towards propulsion R&D towards civilian and strategic sectors.

 

The division has the capability for the Design, Development, Analyses and Testing of Gas Turbine Engine Components: Axial flow compressor stage, Centrifugal and mixed flow compressor stage, Straight and Reverse flow Combustors, Cascades for Compressor and Turbine, Turbines, Heat Transfer, Nozzle, Rotor dynamics and Mechanical aspects and CFD. Over the decades, Propulsion Division has contributed to the needs of GTRE and HAL towards their Gas Turbine Engine Technologies.

 

Contributed towards the development of high speed combustion technologies for DRDO & ISRO.

 

Developed 55 hp Wankel engine for UAV for DRDO..

 

 Carried out collaborative R&D with Private Aerospace Organisatios like Pratt & Whitney   and GE

 

Division continues to support other organizations like DRDO, ADA, ISRO, HAL, IGCAR, DST, BHEL, GE and Honeywell through sponsored projects.


Head

Manjunath P

Joint Head

Rajashekar C

Senior Principal Scientist(2)

Muralidhara H S
Soumendu Jana

Principal Scientist(7)

Ashfaque Ahmad Khan
Dilipkumar Bhanudasji Alone Dr
Monickavasagom Pillai K
Prathapanayaka R
Sathiyamoorthy K
Shobhavathy M T
Venkat S Iyengar Dr

Senior Scientist(8)

Felix J
Giridhara Babu Y
Janaki Rami Reddy M
Sadanand Kulkarni
Senthil Kumaran R
Steve Mithran A J
Veera Sesha Kumar C
Vinod Kumar N

Scientist(13)

Balaji Sankar
BrijeshKumar Shah
Emandi Rajesh
Jayaprakash C
Kishor Kumar
Lakshya Kumar
Manikandan L P
Muthuselvan G
Santhosh Kumar S
Satish Kumar S
Shambhoo
Tahzeeb Hassan Danish
Vijayakrishnan K

Last updated on : 13-12-2017 04:58:46pm