LTS101-850B-2 Turbine

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Family
LTP101
Aircraft Engine Manufacturer
Honeywell
Aircraft Engine Type
Turboshaft
Dry Weight (kg)
128
Length (mm)
789
Height (mm)
644
Width (mm)
470
Fuel
Jet-A1
LP Compressor Stages
0
IP Compressor Stages
0
HP Compressor Stages
2
HP Compressor Technology
1 axial, 1 centrifugal
Combustion Chamber
Annular reverse flow
HP Turbine Stages
1
HP Turbine Technology
axial
IP Turbine Stages
0
LP Turbine Stages
1
LP Turbine Technology
axial
T45 Take Off (°C)
848
T45 Max Continuous (°C)
828
T45OEI30sec (°C)
915
T45OEI2min (°C)
915
T45OEI2min 5 (°C)
892
T45OEI Contiuous (°C)
875
Maximum Takeoff Power (kW)
582
Maximum Continuous Power (kW)
556
OEI2min 30 Power (kW)
625
OEI30min Power (kW)
602
Maximum Takeoff Torque (N·m)
809
Maximum 2min 30 Torque (N·m)
983
Maximum Continuous Torque (N·m)
769
OEI2min 30 Torque (N·m)
872
OEI30min Torque (N·m)
832
HP Take Off Rotation Speed (rpm)
51029
HP Max Continuous Speed (rpm)
50455
HP Transient Speed (rpm)
52178
HPOEI2min Speed (rpm)
51699
HPOEI2min 5 Speed (rpm)
51938
Output Take Off Speed (rpm)
6780
Output Max Continuous Speed (rpm)
6780
Output Transient Speed (rpm)
7380
Output OEI2min Speed (rpm)
6780
Output OEI2min 5 Speed (rpm)
6780
Output Autorotation Speed (rpm)
6780
Output Clockwise Rotation
Yes

Related

142 empty fields

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