RABBIT

100 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

24 lbs thrust

SPECIFICATIONS

Thrust
Idle Thrust
RPM Range
Weight
Diameter
Length
Exhaust Gas Temperature
Fuel Consumption
105 Newtons (24 lbs) @ 152,000 RPM
4.7 Newtons (1 Lbs) @ 42,000 RPM
42,000 – 152,000
1.1 Kg (2.2 Lbs)
91.0 mm (3.58”)
245 mm (10.67”)
500º C – 700º C
0.36 Lt/min (12.2 Oz/min) @152 k
Thrust
105 Newtons (24 lbs) @ 152,000 RPM
Idle Thrust
4.7 Newtons (1 Lbs) @ 42,000 RPM
RPM Range
42,000 – 152,000
Weight
1.1 Kg (2.2 Lbs)
Diameter
91.0 mm (3.58”)
Length
245 mm (10.67”)
Exhaust Gas Temperature
500º C – 700º C
Fuel Consumption
0.36 Lt/min (12.2 Oz/min) @152 k

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