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gptkbp:instanceOf
|
turbojet engine
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gptkbp:aircraft
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gptkb:Hawker_Siddeley_Trident
gptkb:Hawker_Siddeley_748
gptkb:Boeing_787-9
gptkb:Douglas_A-4_Skyhawk
gptkb:Boeing_707
gptkb:Boeing_737-300
gptkb:Boeing_737-500
gptkb:McDonnell_Douglas_DC-8
gptkb:Vickers_VC10
gptkb:Boeing_787-8
gptkb:Boeing_737-400
gptkb:Boeing_720
gptkb:Boeing_787-10
Boeing 757-200
Lockheed L-1011 TriStar
Boeing 767-200
Boeing 737-200
Boeing 777-200
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gptkbp:application
|
military aircraft
civil aircraft
|
|
gptkbp:compressionRatio
|
axial-flow compressor
|
|
gptkbp:coolingSystem
|
air-cooled
|
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gptkbp:developer
|
gptkb:Rolls-Royce_RB.163
|
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gptkbp:diameter
|
3 ft 4 in
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|
gptkbp:emissionsStandard
|
annular combustor
|
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gptkbp:engineConfiguration
|
single-spool
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gptkbp:engineType
|
two-stage turbine
|
|
gptkbp:firstFlight
|
1963
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Rolls-Royce Spey
|
|
gptkbp:is_used_in
|
gptkb:McDonnell_Douglas_F-4_Phantom_II
gptkb:Hawker_Siddeley_Buccaneer
BAC TSR-2
|
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gptkbp:length
|
15 ft 6 in
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce_Limited
|
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gptkbp:notable_feature
|
Spey 202
Spey 301
Spey 512
Spey 555
Spey 600
|
|
gptkbp:propulsion
|
11,000 lbf
|
|
gptkbp:related_engine
|
Brayton_cycle
|
|
gptkbp:replacedBy
|
gptkb:Rolls-Royce_RB.199
|
|
gptkbp:retired
|
1990s
|
|
gptkbp:successor
|
Rolls-Royce RB.183
|
|
gptkbp:type
|
afterburning turbojet
|
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gptkbp:weight
|
1,800 lb
|