Rolls-Royce Nene

Turbojet · Rolls-Royce
Reaction Turbines
Diameter
1257.3 mm
Length
2458.72 mm
Dry Weight
725.7478 kg
Thrust To Weight
3.226

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 9 x 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

No pictures yet for this family.

Airplanes

Name Aircraft Engine Number of Engines Length (m) Flat Wing Span (m) Max Seating
Armstrong Whitworth A.W.52 Rolls-Royce Nene 2 11.4 27.4
Boulton Paul P.111 Rolls-Royce Nene 1 7.9248 7.62
Boulton Paul P.120 Rolls-Royce Nene 1 8.8392 10.0584
Canadair CT-133 Silver Star Rolls-Royce Nene 1 11.48 12.93
Fiat G.80 Rolls-Royce Nene 1 12.93 11.81
FMA IA 36 Cóndor Rolls-Royce Nene 5 34 40
FMA IAe 33 Pulqui II Rolls-Royce Nene 1 11.68 10.6
Rolls-Royce Thrust Measuring Rig Rolls-Royce Nene 2 8.5344
Sud-Est Grognard Rolls-Royce Nene 2 15.4 13.57
Sud-Ouest Espadon Rolls-Royce Nene 1 15 10.6
Supermarine Attacker Rolls-Royce Nene 1 11.43 11.25
Tupolev Tu-12 Rolls-Royce Nene 2 16.45 18.86
All data (15 fields)
Name
Rolls-Royce Nene
Aircraft Engine Manufacturer
Rolls-Royce
Aircraft Engine Type
Turbojet
Dry Weight (kg)
725.7478
Diameter (mm)
1257.3
Length (mm)
2458.72
Wikipedia Article (URL)
en.wikipedia.org/wiki/Rolls-Royce_Nene
Fuel
kerosene
Geared Fan
No
Combustion Chamber
9 x can combustion chambers
Afterburner
No
Streams
1
Thrust To Weight
3.226
Compressor Description
single-stage centrifugal with double-sided impeller
Turbine Description
single-stage axial