Allison J35

Turbojet · Allison
Reaction Turbines
Diameter
939.8 mm
Length
4965.7 mm
Dry Weight
1050.066 kg
Thrust To Weight
2.63

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 eight tubular inter-connected 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 Yes

Pictures

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Airplanes

Name Aircraft Engine Number of Engines Length (m) Flat Wing Span (m)
Convair XB-46 Allison J35 4 32.004 34.4424
Convair XB-53 Allison J35 3 24.2 24.6
Martin XB-48 Allison J35 6 26.14 33.02
North American FJ-1 Fury Allison J35 1 10.3632 11.5824
All data (15 fields)
Name
Allison J35
Aircraft Engine Manufacturer
Allison
Aircraft Engine Type
Turbojet
Dry Weight (kg)
1050.066
Diameter (mm)
939.8
Length (mm)
4965.7
Wikipedia Article (URL)
en.wikipedia.org/wiki/Allison_J35
Fuel
aviation kerosene, JP-4, MIL-F-5624 or 100/130 octane gasoline
Geared Fan
No
Combustion Chamber
eight tubular inter-connected combustion chambers
Afterburner
Yes
Streams
1
Thrust To Weight
2.63
Compressor Description
11-stage axial compressor
Turbine Description
single-stage axial turbine