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2.2 Turbine
Jet Central Turbines utilize a design containing a single shaft turbojet with an annular
combustor. The single stage axial flow turbine drives a single stage centrifugal compressor.
The shaft is supported by 2 fuel/oil lubricated pre-loaded angular contact bearings. The
turbine speed is controlled by the amount of fuel received from the fuel pump, which is
controlled by the POWERPACK / ECU
Turbine Specifications
7 Kg (15.5 Lbs)
Thrust Class
185,000 RPM
@
Full Throttle
0.24 Lt/min
Fuel
(8.1 Oz/min)
Consumption
R.P.M. range
55,000-185,000
500°C - 700°C
E.G.T.
(932 -1292°F)
0.880 Kg
Weight
(1.94 Lbs)
with starter
82 mm
Diameter
(3.228 inches)
232 mm
Length
(9.13 inches)
Bee II
Rabbit 100
10.2 Kg (22.48
Lbs)
152,000
@
RPM
0.36 Lt/min
(12.2 Oz/min)
42,000-152,000
500°C - 700°C
(932 -1292°F)
1.0 Kg
(2.2 Lbs) with
starter
91 mm
(3.582 inches)
245 mm
(9.645 inches)
Cheetah
14 Kg (31 Lbs)
16.3 Kg (36 Lbs)
130,000 RPM
117,000 RPM
@
@
0.47 Lt/min
0.52 Lt/min
(16 Oz/min)
(17.5 Oz/min)
35,000-130,000
32,000-117,000
500°C - 700°C
500°C - 700°C
(932 -1292°F)
(932 -1292°F)
1.360 Kg
1.700 Kg
(3 Lbs)
(3.75 Lbs)
with starter
with starter
102 mm
111 mm
(4 inches)
(4.37 inches)
250 mm
300 mm
(9.842 inches)
(11.8 inches)
Rhino
Mammoth
21.5 Kg (48 Lbs)
104,000 RPM
@
0.70 Lt/min
(23 Oz/min)
28,000-104,000
500°C - 700°C
(932 -1292°F)
2.240 Kg
(4.9 Lbs)
With starter
124 mm
(4.881 inches)
349 mm
(13.74 inches)
9
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