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gptkbp:instance_of
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gptkb:jet_engine
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gptkbp:application
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gptkb:aircraft
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|
gptkbp:certification
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gptkb:civil_aviation_authority
|
|
gptkbp:combustor_type
|
annular combustor
|
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gptkbp:compressor_type
|
axial compressor
|
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gptkbp:control_system
|
hydraulic control system
|
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gptkbp:cooling_system
|
air-cooled
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gptkbp:country_of_origin
|
gptkb:United_Kingdom
|
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gptkbp:design_organization
|
gptkb:Rolls-Royce
|
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gptkbp:diameter
|
3 ft 4 in
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|
gptkbp:engine
|
gptkb:Rolls-Royce_RB.162
advanced materials
air start
|
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gptkbp:engine_configuration
|
twin-spool
|
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gptkbp:engine_type
|
RB.183-01
RB.183-02
RB.183-03
RB.183-04
RB.183-05
RB.183-06
RB.183-07
RB.183-08
RB.183-09
RB.183-10
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|
gptkbp:first_flight
|
gptkb:1960
|
|
gptkbp:fuel_economy
|
0.8 lb/hp/hr
|
|
gptkbp:fuel_type
|
kerosene
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Rolls-Royce RB.183
|
|
gptkbp:introduced
|
1960s
|
|
gptkbp:is_tested_for
|
ground testing
|
|
gptkbp:length
|
12 ft 6 in
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:max_speed
|
Mach 0.9
|
|
gptkbp:noise_level
|
low noise
|
|
gptkbp:notable_feature
|
vectored thrust
|
|
gptkbp:operational_use
|
gptkb:military_aircraft
|
|
gptkbp:propulsion
|
22,000 lbf
|
|
gptkbp:retired
|
1990s
|
|
gptkbp:service
|
5,000 hours
|
|
gptkbp:successor
|
gptkb:Rolls-Royce_RB.199
|
|
gptkbp:turbine_type
|
single-stage turbine
|
|
gptkbp:type
|
gptkb:turbofan_engine
|
|
gptkbp:used_in
|
gptkb:Hawker_Siddeley_Harrier
|
|
gptkbp:weight
|
1,200 lb
|
|
gptkbp:bfsParent
|
gptkb:Rolls-Royce_Spey_800
|
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gptkbp:bfsLayer
|
6
|