The Jet Fuel Starter (JFS) for starting the main engine of Light Combat Aircraft (LCA) is a twin shaft gas turbine consisting of a centrifugal compressor driven by an axial turbine, reverse flow combustor, digital electronic fuel control system and a free power turbine that supplies the motive power for starting the LCA engine.
Main Characteristics
| Main Characteristics | |
|---|---|
| Intake Diameter (m) | 0.29 |
| Length (m) | 0.64 |
| Weight (kg) | 52 |
| Power(kw) | 110 |
