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gptkbp:instance_of
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gptkb:engine
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gptkbp:bfsLayer
|
5
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gptkbp:bfsParent
|
gptkb:Westland_Sea_King
gptkb:Sea_King_helicopter
gptkb:Sea_King_helicopters
gptkb:Westland_Wessex
gptkb:Sea_King_HAS.1
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gptkbp:application
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gptkb:aircraft
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gptkbp:controls
|
hydraulic control system
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gptkbp:cooling_system
|
air-cooled
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gptkbp:design
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gptkb:Rolls-Royce
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gptkbp:developer
|
1940s to 1950s
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gptkbp:diameter
|
3 ft 6 in
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gptkbp:engine
|
gptkb:Rolls-Royce_RB.163
gptkb:Rolls-Royce_Dart
gptkb:Rolls-Royce_Avon
gptkb:Rolls-Royce_RB.108
gptkb:Rolls-Royce_RB.145
high reliability
pylon-mounted
influenced future designs
good performance for its time
moderate efficiency
used in various military aircraft
air-start system
turbojet engine configuration
early turbojet technology
approximately 3,000 hours
developed during the Cold War era
part of Rolls-Royce's heritage in aviation engineering
subject of research and development projects.
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gptkbp:engine_type
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axial
single-stage
compatible with various airframes
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|
gptkbp:first_flight
|
1950
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gptkbp:fuel_type
|
annular
kerosene
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Rolls-Royce Gnome
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gptkbp:impact
|
significant impact on jet propulsion technology
|
|
gptkbp:length
|
12 ft 6 in
|
|
gptkbp:maintenance
|
moderate maintenance requirements
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce_Limited
|
|
gptkbp:noise_level
|
high noise level
|
|
gptkbp:operational_area
|
gptkb:battle
|
|
gptkbp:predecessor
|
gptkb:Rolls-Royce_Derwent
|
|
gptkbp:propulsion
|
5,000 lbf
|
|
gptkbp:successor
|
gptkb:Rolls-Royce_Spey
|
|
gptkbp:type
|
turbojet
|
|
gptkbp:used_in
|
gptkb:Hawker_Siddeley_Buccaneer
gptkb:de_Havilland_Sea_Vixen
|
|
gptkbp:variant
|
gptkb:Gnome_Mk_101
gptkb:Gnome_Mk_102
gptkb:Gnome_Mk_103
gptkb:Gnome_Mk_104
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|
gptkbp:weight
|
1,200 lb
|