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RHINO
200 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
45 lbs thrust
SPECIFICATIONS
Thrust
Idle Thrust
RPM Range
Weight
Diameter
Length
Exhaust Gas Temperature
Fuel Consumption
200 Newtons (45 Lbs) @ 121,000 RPM
6 Newtons (1.34 Lbs) @ 32,000 RPM
32,000 – 121,000
1.78 Kg (3.93 Lbs)
111.0 mm (4.37”)
302 mm (11.89”)
500º C – 700º C
0.55 Lt/min (19.5 Oz/min) @121 k
Thrust
200 Newtons (45 Lbs) @ 121,000 RPM
Idle Thrust
6 Newtons (1.34 Lbs) @ 32,000 RPM
RPM Range
32,000 – 121,000
Weight
1.78 Kg (3.93 Lbs)
Diameter
111.0 mm (4.37”)
Length
302 mm (11.89”)
Exhaust Gas Temperature
500º C – 700º C
Fuel Consumption
0.55 Lt/min (19.5 Oz/min) @121 k
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02630
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