A turbine with a class of its own, 11 kg (24 lbs) of thrust, a weight of only 2.2 lbs and the fastest acceleration ever…
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.
 
Category
22.4 Lbs. thrust
 
Specifications
Thrust: 100 Newtons, 10.20 kg (22.48 lbs) @ 152,000 RPM
Idle Thrust: 0.4 kg (0.90 lbs)
RPM Range: 42,000 – 152,000
Weight: 1.0 kg (2.20 lbs) with starter
Diameter: 91 mm (3.58 in)
Length: 228 mm (8.98 in) with starter
Exhaust Gas Temperature: 500º C – 700º C
Fuel Consumption: 0.36 lt/min (12.67 oz/min) @ 152,000 RPM
 
For more options and paint schemes available visit:
https://sites.google.com/site/jetcentralus/home/turbines/rabbit
 
Prices do not include shipping and local taxes.