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gptkbp:instanceOf
|
jet engine
|
|
gptkbp:airlines
|
60 lb/s
|
|
gptkbp:application
|
military aircraft
|
|
gptkbp:built
|
gptkb:Cold_War
|
|
gptkbp:controls
|
hydraulic control system
|
|
gptkbp:coolingSystem
|
air-cooled
direct air cooling
|
|
gptkbp:developer
|
5 years
|
|
gptkbp:diameter
|
3 ft 4 in
|
|
gptkbp:displacement
|
significant in military aviation.
|
|
gptkbp:engine
|
aluminum alloy
modular design
rear-mounted
influenced future designs
2,000 hours
early jet technology
roller bearings
|
|
gptkbp:engineConfiguration
|
single_spool
|
|
gptkbp:engineType
|
electric starter
axial compressor
single-stage turbine
|
|
gptkbp:firstRace
|
1958
|
|
gptkbp:fuel_capacity
|
moderate
|
|
gptkbp:fuelType
|
kerosene
annular combustion chamber
|
|
gptkbp:future_plans
|
flight testing
ground testing
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Rolls-Royce RB.163
|
|
gptkbp:is_used_in
|
gptkb:Hawker_Siddeley_Harrier
|
|
gptkbp:length
|
12 ft 6 in
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:noise_level
|
high
|
|
gptkbp:notable_feature
|
RB.163-1
RB.163-2
RB.163-3
|
|
gptkbp:operational_status
|
gptkb:vertical_takeoff_and_landing_(VTOL)_aircraft
|
|
gptkbp:performances
|
high thrust-to-weight ratio
|
|
gptkbp:produces
|
over 1,000
|
|
gptkbp:productionYears
|
1960
1970
|
|
gptkbp:propulsion
|
22,000 lbf
18.3:1
|
|
gptkbp:related_engine
|
gptkb:Rolls-Royce_RB.162
gptkb:Rolls-Royce_RB.168
|
|
gptkbp:reliability
|
high
|
|
gptkbp:successor
|
gptkb:Rolls-Royce_RB.162
|
|
gptkbp:type
|
turbojet engine
|
|
gptkbp:weight
|
1,200 lb
|