Rolls-Royce Derwent

Turbojet · Rolls-Royce
Reaction Turbines
Diameter
1092.2 mm
Length
2133.6 mm
Dry Weight
442.2526 kg
Thrust To Weight
2.04
Specific Fuel Consumption
33.14 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 10 × can 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

Pictures

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Airplanes

Name Aircraft Engine Number of Engines Length (m) Flat Wing Span (m)
Avro 707 Rolls-Royce Derwent 1 12.8016 10.3632
FMA I.Ae. 37 Rolls-Royce Derwent 1 11.78 10
Fokker S.14 Machtrainer Rolls-Royce Derwent 1 13.3 12
Short SB.5 Rolls-Royce Derwent 1 13.94 10.9
All data (16 fields)
Name
Rolls-Royce Derwent
Aircraft Engine Manufacturer
Rolls-Royce
Aircraft Engine Type
Turbojet
Dry Weight (kg)
442.2526
Diameter (mm)
1092.2
Length (mm)
2133.6
Wikipedia Article (URL)
en.wikipedia.org/wiki/Rolls-Royce_Derwent
Fuel
Kerosene
Geared Fan
No
Combustion Chamber
10 × can combustion chambers
Afterburner
No
Streams
1
Thrust To Weight
2.04
Specific Fuel Consumption (g/(kN·s))
33.14
Compressor Description
Single-stage double-sided centrifugal compressor
Turbine Description
Single-stage axial