|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
helicopter propulsion
|
|
gptkbp:combustor_type
|
annular combustion chamber
|
|
gptkbp:compressor_type
|
centrifugal compressor
|
|
gptkbp:control_system
|
hydromechanical control system
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design
|
gptkb:Rolls-Royce_Limited
|
|
gptkbp:diameter
|
1.5 ft
|
|
gptkbp:emissions_standard
|
ICAO Chapter 3
|
|
gptkbp:engine
|
Brayton cycle
air start
single shaft
|
|
gptkbp:engine_configuration
|
inline engine
|
|
gptkbp:first_flight
|
gptkb:1960
|
|
gptkbp:fuel_economy
|
0.5 lb/hp/hr
|
|
gptkbp:fuel_type
|
kerosene
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Rolls-Royce RB162
|
|
gptkbp:length
|
3.4 ft
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:max_speed
|
0.85 Mach
|
|
gptkbp:noise_level
|
low noise
|
|
gptkbp:operational_history
|
1960s to 1970s
|
|
gptkbp:power_output
|
1,100 k W
|
|
gptkbp:propulsion
|
3.75
1,500 lbf
|
|
gptkbp:related_aircraft
|
gptkb:Westland_Wessex
|
|
gptkbp:service_ceiling
|
15,000 ft
|
|
gptkbp:turbine_type
|
axial turbine
|
|
gptkbp:type
|
turbojet
|
|
gptkbp:used_in
|
gptkb:Bristol_Belvedere
|
|
gptkbp:weight
|
400 lb
|
|
gptkbp:bfsParent
|
gptkb:Hawker_Siddeley_Kestrel
|
|
gptkbp:bfsLayer
|
6
|