|
gptkbp:instanceOf
|
jet engine
|
|
gptkbp:aircraft
|
strategic bomber
|
|
gptkbp:controls
|
hydraulic
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:design_feature
|
low bypass ratio
|
|
gptkbp:diameter
|
3 ft 6 in
|
|
gptkbp:emissionsStandard
|
standard
|
|
gptkbp:engine
|
1,500 kg
military aircraft
1.1 m
3.8 m
modular
RB.153
Rolls-Royce_design_team
|
|
gptkbp:engineConfiguration
|
twin-spool
|
|
gptkbp:engineType
|
turbojet
axial
air-start
|
|
gptkbp:fanBase
|
single stage
|
|
gptkbp:firstRace
|
1955
|
|
gptkbp:fuel_capacity
|
high
moderate
|
|
gptkbp:fuelType
|
annular
spark plug
kerosene
|
|
gptkbp:hasArea
|
ground test
|
|
gptkbp:historical_significance
|
first British turbofan engine
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Rolls-Royce RB.153
|
|
gptkbp:is_used_in
|
Avro Vulcan
|
|
gptkbp:length
|
12 ft 6 in
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:maximum_speed
|
Mach_0.9
|
|
gptkbp:noise_level
|
high
|
|
gptkbp:notable_feature
|
afterburner
|
|
gptkbp:operational_status
|
military aviation
|
|
gptkbp:operationalRange
|
1,500 miles
|
|
gptkbp:produces
|
200
|
|
gptkbp:productionYears
|
1950s
1955-1965
|
|
gptkbp:propulsion
|
7.3
22,000 lbf
98 kN
|
|
gptkbp:related_engine
|
gptkb:Rolls-Royce_RB.162
|
|
gptkbp:reliability
|
high
|
|
gptkbp:retirementYear
|
1980s
|
|
gptkbp:service_ceiling
|
40,000 ft
|
|
gptkbp:serviceType
|
1960s
|
|
gptkbp:successor
|
gptkb:Rolls-Royce_RB.162
gptkb:Rolls-Royce_RB.211
|
|
gptkbp:team
|
Rolls-Royce_engineers
|
|
gptkbp:type
|
turbofan engine
|
|
gptkbp:weight
|
3,000 lb
|