Avro Canada Orenda

Turbojet · Avro Canada
Reaction Turbines
Diameter
1066.8 mm
Length
3086.354 mm
Dry Weight
1102.229 kg
Thrust To Weight
3.09
Specific Fuel Consumption
25.492 g/(kN·s)

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 can type, 6
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)
Avro Canada CF-103 Avro Canada Orenda 2 17.9832 13.1064
Canadair Sabre Avro Canada Orenda 1 11.4422 11.3142
All data (16 fields)
Name
Avro Canada Orenda
Aircraft Engine Manufacturer
Avro Canada
Aircraft Engine Type
Turbojet
Dry Weight (kg)
1102.229
Diameter (mm)
1066.8
Length (mm)
3086.354
Wikipedia Article (URL)
en.wikipedia.org/wiki/Avro_Canada_Orenda
Fuel
JP-1 or JP-4
Geared Fan
No
Combustion Chamber
can type, 6
Afterburner
No
Streams
1
Thrust To Weight
3.09
Specific Fuel Consumption (g/(kN·s))
25.492
Compressor Description
10-stage axial flow
Turbine Description
two-stage axial flow