Lynx

130 SE Series

The Jet Central turbines 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

29.22 Lbs. of thrust

Specifications

Thrust 130 Newtons (29.22 lbs) @ 130,000 RPM
Idle Thrust 4.2 Newtons (0.94 lbs) @ 35,000 RPM
RPM Range 35,000 – 130,000
Weight 1.29 kg (2.84 lbs)
Diameter 99 mm (3.9 in)
Length 229 mm (9.02 in)
Exhaust Gas Temperature 500º C – 700º C
Fuel Consumption 365.5 g/min (0.43 lt/min) (15.13 oz/min) @ 130,000 RPM