Armstrong Siddeley Sapphire

Diameter
953.77 mm
Length
3180.08 mm
Dry Weight
1383.457 kg
Thrust To Weight
3.607
Specific Fuel Consumption
0.885 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 Annular with 24 hockey-stick vaporisers
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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All data (16 fields)
Name
Armstrong Siddeley Sapphire
Aircraft Engine Manufacturer
Armstrong Siddeley
Aircraft Engine Type
Turbojet
Dry Weight (kg)
1383.457
Diameter (mm)
953.77
Length (mm)
3180.08
Wikipedia Article (URL)
en.wikipedia.org/wiki/Armstrong_Siddeley_Sapphire
Fuel
Aviation kerosene
Geared Fan
No
Combustion Chamber
Annular with 24 hockey-stick vaporisers
Afterburner
No
Streams
1
Thrust To Weight
3.607
Specific Fuel Consumption (g/(kN·s))
0.885
Compressor Description
13-stage axial flow
Turbine Description
Two-stage