|
gptkbp:instanceOf
|
turbojet engine
|
|
gptkbp:application
|
military aircraft
|
|
gptkbp:controls
|
hydromechanical control
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:developer
|
gptkb:Rolls-Royce_RB.108
|
|
gptkbp:diameter
|
3 ft 4 in
|
|
gptkbp:engine
|
1
influential in jet engine design.
British_design
|
|
gptkbp:engineConfiguration
|
twin-spool
produced in large numbers
|
|
gptkbp:engineType
|
axial compressor
single-stage turbine
several variants
|
|
gptkbp:exhaustSystem
|
variable geometry
|
|
gptkbp:firstFlight
|
1958
|
|
gptkbp:fuel_capacity
|
0.85 lb/lbf/hr
|
|
gptkbp:fuelType
|
kerosene
annular combustion chamber
|
|
gptkbp:hasArea
|
extensive testing
civil and military certification
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Rolls-Royce RB.162
|
|
gptkbp:is_used_in
|
gptkb:Hawker_Siddeley_Harrier
|
|
gptkbp:length
|
12 ft 6 in
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:maximum_speed
|
Mach_0.9
|
|
gptkbp:noise_level
|
low noise
|
|
gptkbp:notableUsers
|
gptkb:Royal_Air_Force
gptkb:United_States_Marine_Corps
|
|
gptkbp:performances
|
high reliability
good performance
moderate maintenance
|
|
gptkbp:propulsion
|
4.17
5,000 lbf
|
|
gptkbp:related_engine
|
Brayton_cycle
|
|
gptkbp:retirementYear
|
1980s
|
|
gptkbp:serviceType
|
1960
|
|
gptkbp:successor
|
gptkb:Rolls-Royce_RB.199
|
|
gptkbp:type
|
afterburning turbojet
|
|
gptkbp:updates
|
upgraded versions available
|
|
gptkbp:weight
|
1,200 lb
|