Activities
Design & Analysis
AirFrame
AirCraft Materials
Aero Dynamics
Avionics & Electrical Systems
Propulsion
Weapon Systems
Testing & Qualification
Avionics&Flight Control
Simulation
Weapon System
Flight Testing
LCA Production
Workcenters Activities
Variants
GE F404-F2J3
Kaveri
JFS
Engine Test Facility
Gas Turbine Research Establishment is carrying out the design and development of the KAVERI engine for powering he Light Combat Aircraft (LCA).
Kaveri engine is a flat rated two spool turbofan engine
Air mass flow :
75.00 kg/sec
By pass ratio :
0.161
Overall pressure ratio :
21.00
TET :
1480 deg – 1688 deg K
Max (Dry) thrust :
50.6 kN
Max ( Reheat) :
21.56 gm/s/kN
SFC (max reheat) :
54.52 gm/kg/sec
Copyright @ 2001-2003, Aeronautical Development Agency, Bangalore
Aeronautical Development Agency, Ministry of Defence, Govt. of India, P.B.No: 1718, Vimanapura Post, Bangalore 560017, India
Comments and Suggestions to WebMaster : vponraj@jetmail.ada.gov.in, ramki@jetmail.ada.gov.in
Visitor No :
FastCounter by bCentral
