Allison J33

Turbojet · Allison
Reaction Turbines
Diameter
1282.7 mm
Length
2717.8 mm
Dry Weight
825.5381 kg
Thrust To Weight
2.53

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 14 can type stainless steel combustion chambers
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

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Airplanes

Name Aircraft Engine Number of Engines Length (m) Flat Wing Span (m)
Lockheed T2V SeaStar Allison J33 1 11.75 13.06
All data (15 fields)
Name
Allison J33
Aircraft Engine Manufacturer
Allison
Aircraft Engine Type
Turbojet
Dry Weight (kg)
825.5381
Diameter (mm)
1282.7
Length (mm)
2717.8
Wikipedia Article (URL)
en.wikipedia.org/wiki/Allison_J33
Fuel
JP-4, Kerosene (AN-F-32) or 100/130 gasoline
Geared Fan
No
Combustion Chamber
14 can type stainless steel combustion chambers
Afterburner
No
Streams
1
Thrust To Weight
2.53
Compressor Description
single-stage double-sided centrifugal compressor
Turbine Description
single-stage axial