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gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:aircraft_operated
|
gptkb:Bristol_F.2_Fighter
|
|
gptkbp:application
|
biplanes
|
|
gptkbp:compression_ratio
|
5.5:1
|
|
gptkbp:configuration
|
liquid-cooled
|
|
gptkbp:cooling_system
|
water-cooled
|
|
gptkbp:displacement
|
22.5 liters
|
|
gptkbp:engine
|
four-stroke
|
|
gptkbp:first_introduced
|
1915
|
|
gptkbp:fuel_capacity
|
800 mm
1,200 mm
|
|
gptkbp:fuel_type
|
aviation gasoline
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Rolls-Royce 150 HP
|
|
gptkbp:ignition_system
|
magneto ignition
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce_Limited
|
|
gptkbp:notable_users
|
gptkb:Royal_Flying_Corps
|
|
gptkbp:number_of_engines
|
V configuration
|
|
gptkbp:powers
|
150 horsepower
|
|
gptkbp:produces
|
approximately 1,000 units
|
|
gptkbp:production_years
|
1915-1925
|
|
gptkbp:propulsion
|
0.375 hp/lb
|
|
gptkbp:replaced_by
|
gptkb:Rolls-Royce_Kestrel
|
|
gptkbp:successor
|
gptkb:Rolls-Royce_Eagle
|
|
gptkbp:type
|
gptkb:V8_engine
|
|
gptkbp:used_in
|
gptkb:military_aircraft
|
|
gptkbp:valve_configuration
|
overhead valves
|
|
gptkbp:variant
|
gptkb:Rolls-Royce_150_HP_(A)
|
|
gptkbp:weight
|
approximately 400 lb
|
|
gptkbp:bfsParent
|
gptkb:Sir_Henry_Royce
|
|
gptkbp:bfsLayer
|
5
|