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The JET CENTRAL TURBINES ENGINES are in its own right a single stage centrifugal flow gas turbine engine, configured to operate as a TURBOJET ENGINE for use mainly, but not exclusively, in remotely piloted fixed wing aircraft. Such aircraft and their control systems must be appropriately designed and constructed to be compatible with the performance of the TURBOJET ENGINE.
18 Lbs. thrust
Thrust: 8.2 kg (18 lbs) @ 178,000 RPM
Idle Thrust: 0.38 kg (0.8 lbs)
RPM Range: 55,000 – 178,000
Weight: 0.790 kg (1.74 lbs) with starter
Diameter: 82 mm (3.23 in)
Length: 221 mm (8.7 in) with starter
Exhaust Gas Temperature: 500º C – 700º C (932ª F – 1292ª F)
Fuel Consumption: 0.335 lt/min (11.79 oz/min) @ 130,000 RPM