Pratt & Whitney J52

Turbojet · Pratt & Whitney
Reaction Turbines
Diameter
965.2 mm
Length
2997.2 mm
Dry Weight
1051.427 kg
Thrust To Weight
4.83

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 —
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

No pictures yet for this family.

Airplanes

Name Aircraft Engine Number of Engines Length (m) Flat Wing Span (m)
Grumman A-6 Intruder Pratt & Whitney J52 2 16.4592 16.1544
Lockheed Martin A-4AR Fightinghawk Pratt & Whitney J52 1 12.3 8.38
McDonnell Douglas A-4G Skyhawk Pratt & Whitney J52 1 12.27 8.38
All data (14 fields)
Name
Pratt & Whitney J52
Aircraft Engine Manufacturer
Pratt & Whitney
Aircraft Engine Type
Turbojet
Dry Weight (kg)
1051.427
Diameter (mm)
965.2
Length (mm)
2997.2
Wikipedia Article (URL)
en.wikipedia.org/wiki/Pratt_%26_Whitney_J52
Fuel
JP-4
Geared Fan
No
Afterburner
No
Streams
1
Thrust To Weight
4.83
Compressor Description
axial flow, 5-stage LP, 7-stage HP
Turbine Description
single stage HP, single stage LP