Initial Operational Capability (IOC):
Also Known As: Small Turbofan Engine
Parent System: STFE
Initial Operational Capability (IOC): 2022
Maiden Flight: 2019
Total Production: ?
There are no reviews so far
Description: The Small Turbofan Engine (STFE) is a new engine being developed by India to power subsonic Unmanned Aerial Vehicles (UAVs) as well as long-range cruise missiles such as Nirbhay. The engine features a maximum thrust of 400 kilograms with 95 percent of components being produced domestically in India. The engine is intended to operate at altitudes of up to 30,000-ft (10,000 meters). The engine is expected to enter the flight test program in the first half of 2019.
Max Takeoff Thrust: 400 kilogram (882 pound)
CEP: Circular Error Probable
Meters (m) Kilometers (km) Nautic Miles (nm) Inch (in) Yard (yd) Foot (ft) Millimeter (mm)
Pound (lb) Kilogram (kg) kN (KiloNewton) Ton (t)
Meters per Second (mps) Kilometers per Hour (kph) Knot (kt) Miles per Hour (mph)
Liter (l) Galon (gl)
Year (yr) Minutes (min) Second (sec)
There is 1 news
on 22 Apr 2019
Operators & Related Equipment
Grand Total ?1
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