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Type sheet: rrderw8

Rolls Royce Derwent 8
Jet Engine, United Kingdom

[Technical Data] [Expo/Images] - [ Rolls Royce] [ Jet Engines 1946-1974]


Thrust :

1630 kp

1630 kp


Diameter :

413.39 in

1050.00 mm


Compressor :

Centrifugal Compressor


Combustiuon Chambers :

9 Combustion Chambers


Discharger :

Single Stage Turbine


Air flow :

62.84 lbs

28.50 kg/sec


Compression :




Performance data

Max. r.p.m. :

14700.00 r.p.m.

14700.00 U/min


Max. power output :

1630 kp

1630 kp



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The Virtual Aviation Museum
european aviation history on the Internet
Thomas Wilberg ©

TW/01/04/06 09:27:48