General Electric J97

Turbojet · General Electric Company
Reaction Turbines
Maximum Takeoff Thrust
23.4 kN
Diameter
619.76 mm
Length
2781.3 mm
Dry Weight
314.7931 kg
Thrust To Weight
11.5

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
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 Yes

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All data (16 fields)
Name
General Electric J97
Aircraft Engine Manufacturer
General Electric Company
Aircraft Engine Type
Turbojet
Dry Weight (kg)
314.7931
Diameter (mm)
619.76
Length (mm)
2781.3
Wikipedia Article (URL)
en.wikipedia.org/wiki/General_Electric_J97
Geared Fan
No
Combustion Chamber
annular
Afterburner
Yes
Streams
1
Maximum Takeoff Thrust (kN)
23.4
Thrust To Weight
11.5
Afterburner Thrust (kN)
35
Compressor Description
14-stage
Turbine Description
two-stage