General Electric CJ610

Turbojet · General Electric Company
Reaction Turbines
Diameter
449.58 mm
Length
1297.94 mm
Dry Weight
189.148 kg
Thrust To Weight
7.4
Specific Fuel Consumption
27.758 g/(kN·s)

Architecture

Fan Fan Stages — Fan Blades — Fan Technology — Fan Pressure Ratio —
Gearbox Geared Fan No Gear — Reduction Ratio —
LP compressor Low-Pressure Compressor Stages — Low-Pressure Compressor Technology — BP Compressor Pressure Ratio —
IP compressor Intermediary-Pressure Compressor Stages — Intermediary-Pressure Compressor Technology — IP Compressor Pressure Ratio —
HP compressor High-Pressure Compressor Stages — High-Pressure Compressor Technology — HP Compressor Pressure Ratio —
Combustor Combustion Chamber Annular combustion chamber
HP turbine High Pressure Compressor Stages — High-Pressure Turbine Technology —
IP turbine Intermediary-Pressure Turbine Stages — Intermediary-Pressure Turbine Technology —
LP turbine Low-Pressure Turbine Stages — Low-Pressure Turbine Technology —
Whole engine Streams 1 Bypass Ratio — Overall Pressure Ratio — Afterburner No

Pictures

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Airplanes

Name Aircraft Engine Number of Engines Length (m) Flat Wing Span (m) Max Seating
Bede BD-10 General Electric CJ610 1 8.794 6.55 1
Learjet 24 General Electric CJ610 2 13.1064 10.668 6
Learjet 25 General Electric CJ610 2 14.3256 10.668 8
Viper Aircraft ViperJet General Electric CJ610 1 7.8 8.48 1
All data (15 fields)
Name
General Electric CJ610
Aircraft Engine Manufacturer
General Electric Company
Aircraft Engine Type
Turbojet
Dry Weight (kg)
189.148
Diameter (mm)
449.58
Length (mm)
1297.94
Wikipedia Article (URL)
en.wikipedia.org/wiki/General_Electric_CJ610
Geared Fan
No
Combustion Chamber
Annular combustion chamber
Afterburner
No
Streams
1
Thrust To Weight
7.4
Specific Fuel Consumption (g/(kN·s))
27.758
Compressor Description
8-stage axial flow
Turbine Description
2-stage