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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 built to be compatible with the performance of the Turbojet engine.
CATEGORY
29.22 lbs thrust
SPECIFICATIONS
Thrust
Idle Thrust
RPM Range
Weight
Diameter
Length
Exhaust Gas Temperature
Fuel Consumption
130 Newtons (29.22 Lbs) @ 130,000 RPM
4.2 Newtons (0.94 Lbs) @ 35,000 RPM
35,000 – 130,000
1.29 Kg (2.84 Lbs)
99.0 mm (3.90”)
229 mm (9.02”)
500º C – 700º C
0.43 Lt/min (15.13 Oz/min) @130 k
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
99.0 mm (3.90”)
Length
229 mm (9.02”)
Exhaust Gas Temperature
500º C – 700º C
Fuel Consumption
0.43 Lt/min (15.13 Oz/min) @130 k
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