F-86's J47 WATER-INJECTION TURBOJET OPERATION DATA AND maintenance manual

[m13katyusa2020]

F-86's J47 WATER-INJECTION TURBOJET OPERATION DATA AND maintenance manual.
General characteristics Type: turbojet (/wiki-Turbojet)
Length: 145 inches (370 cm) (with tailcone)
Diameter: 36.75 inches (93.3 cm) maximum
Dry weight: 2,554 pounds (1,158 kg) dry, equipped Components
Compressor: 12-stage axial compressor (/wiki-Axial_compressor)
Turbine (/wiki-Turbine): single-stage axial
Fuel type: JP-1 (/wiki-JP-1), JP-2 (/wiki-Jet_fuel#Military_jet_fuels), JP-3 (/wiki-JP-3), JP-4 (/wikiJP-4) or MIL-F-5572 gasoline
Oil system: pressure feed spray with scavenge Performance
Maximum thrust (/wiki-Thrust): 5,970 lbf (26.56 kN) at 7950 rpm ; 6,970 lbf (31.00 kN) with water injection
Overall pressure ratio (/wiki-Overall_pressure_ratio): 5.35
Air mass flow: 92 lb/s (42 kg/s)
Specific fuel consumption (/wiki-Thrust_specific_fuel_consumption): 1.014 lb/(lbf⋅h) (28.7 g/(kN⋅s))
Thrust-to-weight ratio (/wiki-Thrust-to-weight_ratio): 2.34 at take-off dry power

Added: J47 Operation Manual thanks to mikejohnson96:

J47OperationandServicing

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Please download the following pdf attachment:

 

[m13katyusa2020]

F-86's J47 WATER-INJECTION TURBOJET OPERATION DATA AND maintenance manual.
General characteristics Type: turbojet (/wiki-Turbojet)
Length: 145 inches (370 cm) (with tailcone)
Diameter: 36.75 inches (93.3 cm) maximum
Dry weight: 2,554 pounds (1,158 kg) dry, equipped Components
Compressor: 12-stage axial compressor (/wiki-Axial_compressor)
Turbine (/wiki-Turbine): single-stage axial
Fuel type: JP-1 (/wiki-JP-1), JP-2 (/wiki-Jet_fuel#Military_jet_fuels), JP-3 (/wiki-JP-3), JP-4 (/wikiJP-4) or MIL-F-5572 gasoline
Oil system: pressure feed spray with scavenge Performance
Maximum thrust (/wiki-Thrust): 5,970 lbf (26.56 kN) at 7950 rpm ; 6,970 lbf (31.00 kN) with water injection
Overall pressure ratio (/wiki-Overall_pressure_ratio): 5.35 Air mass flow: 92 lb/s (42 kg/s)
Specific fuel consumption (/wiki-Thrust_specific_fuel_consumption): 1.014 lb/(lbf⋅h) (28.7 g/(kN⋅s))
Thrust-to-weight ratio (/wiki-Thrust-to-weight_ratio): 2.34 at take-off dry power
View attachment 670609

For materials of the engine, refer to Basic Aircraft Materials and treatment:

Basic Aircraft materials chemical composition, treatment and properties books and manuals thread

Public free Manuals: 1st pdf attachment was published by the navy for the basic training of the chemical composition and treatment of aircraft metal. 2nd pdf attachment was published by the navy for the basic training of the chemical composition and treatment of ship metal. 3rd pdf attachment...

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