Wright J65

Turbojet · Wright
Reaction Turbines
Diameter
953.008 mm
Length
3098.8 mm
Dry Weight
1259.172 kg
Thrust To Weight
2.61

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 No

Pictures

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Airplanes

Name Aircraft Engine Number of Engines Length (m) Flat Wing Span (m) Max Seating
Curtiss Teal Wright J65 1 9.22 13.87
Martin B-57 Canberra Wright J65 2 20 19.5
North American FJ-4 Fury Wright J65 1 11.1 11.9
Republic F-84F Thunderstreak Wright J65 1 13.23 10.25
Travel Air 4000 Wright J65 1 7.3152 10.0584 2
All data (14 fields)
Name
Wright J65
Aircraft Engine Manufacturer
Wright
Aircraft Engine Type
Turbojet
Dry Weight (kg)
1259.172
Diameter (mm)
953.008
Length (mm)
3098.8
Wikipedia Article (URL)
en.wikipedia.org/wiki/Wright_J65
Geared Fan
No
Combustion Chamber
annular
Afterburner
No
Streams
1
Thrust To Weight
2.61
Compressor Description
Single-spool 13-stage axial
Turbine Description
2-stage axial