Type: Coupled Turboshaft
Length: 65.3 in (1,660 mm)
Nominal Diameter: 19 in (480 mm) (each gas generator)
Weight: 617 lb (280 kg)
Compressor: 3-stage axial and 1-stage centrifugal (each gas generator)
Combustors: Reverse flow annular combustor
Turbine: 1-stage gas generator turbine + 1-stage free-power turbine (each gas generator)
Maximum Power: 1,800 shp (1,300 kW) at 33,000 free-power turbine rpm: flat-rated to 1,290 shp (960 kW)
Overall Pressure Ratio: 7.2:1
Turbine inlet temperature: NA
Power-to-weight ratio: 2.92 shp/lb (4.80 kW/kg)
Variants
Data in progress.
Aircraft
UH-1N
Bell 212
Bell 412
AH-1T
