|
gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:application
|
gptkb:military_aircraft
|
|
gptkbp:compression_ratio
|
6.5:1
|
|
gptkbp:configuration
|
14-cylinder
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:country_of_origin
|
gptkb:United_Kingdom
|
|
gptkbp:displacement
|
1,000 cubic inches
|
|
gptkbp:engine
|
used in various aircraft models.
|
|
gptkbp:engine_accessories
|
gptkb:Racing
|
|
gptkbp:engine_bore
|
5.5 inches
|
|
gptkbp:engine_configuration
|
horizontally opposed
cradle mount
|
|
gptkbp:engine_power
|
high
excellent
1,000 hp at 2,500 rpm
|
|
gptkbp:engine_starting_system
|
electric starter
|
|
gptkbp:engine_stroke
|
6.0 inches
|
|
gptkbp:engine_type
|
piston engine
|
|
gptkbp:exhaust_system
|
exhaust stacks
|
|
gptkbp:fuel_capacity
|
3.5 feet
2.5 feet
3.0 feet
|
|
gptkbp:fuel_economy
|
0.5 lb/hp/hr
|
|
gptkbp:fuel_type
|
aviation gasoline
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Bristol Pegasus I. M.3
|
|
gptkbp:ignition_system
|
spark ignition
|
|
gptkbp:introduced_in
|
1936
|
|
gptkbp:maintenance
|
periodic overhaul
|
|
gptkbp:manufacturer
|
gptkb:Bristol_Aeroplane_Company
|
|
gptkbp:noise_level
|
low
85 d B
|
|
gptkbp:number_of_produced_units
|
over 10,000
|
|
gptkbp:original_run
|
1936
|
|
gptkbp:power_output
|
1,000 horsepower
|
|
gptkbp:propeller
|
variable-pitch propeller
|
|
gptkbp:retired
|
1960s
|
|
gptkbp:successor
|
gptkb:Bristol_Centaurus
|
|
gptkbp:torque
|
1,200 lb-ft
|
|
gptkbp:type
|
gptkb:radial_engine
|
|
gptkbp:used_in
|
gptkb:Bristol
gptkb:Bristol_Beaufighter
|
|
gptkbp:valve_configuration
|
pushrod
|
|
gptkbp:variant
|
Pegasus XX
Pegasus XXX
|
|
gptkbp:weight
|
1,200 pounds
|
|
gptkbp:bfsParent
|
gptkb:Bristol_Type_226
|
|
gptkbp:bfsLayer
|
7
|