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gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:application
|
gptkb:military_aircraft
civil aircraft
|
|
gptkbp:compression_ratio
|
6.5:1
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:country_of_origin
|
gptkb:United_Kingdom
|
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gptkbp:cylinder_configuration
|
14-cylinder
|
|
gptkbp:displacement
|
2,000 cubic inches
|
|
gptkbp:engine_configuration
|
various
radial
|
|
gptkbp:engine_power
|
high
2,000 hp
1,600 hp
1,500 hours
2,500 rpm
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|
gptkbp:engine_type
|
gptkb:Hercules_2000
gptkb:Hercules_3000
gptkb:Hercules_4000
gptkb:Hercules_5000
gptkb:Hercules_6000
gptkb:Hercules_7000
gptkb:Hercules_8000
gptkb:Hercules_9000
piston engine
Hercules 1000
Hercules 10000
|
|
gptkbp:exhaust_system
|
single exhaust
|
|
gptkbp:fuel_capacity
|
3 ft 6 in
1,200 lb
4 ft 9 in
|
|
gptkbp:fuel_economy
|
0.5 lb/hp/hr
|
|
gptkbp:fuel_type
|
aviation gasoline
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Bristol Hercules
|
|
gptkbp:ignition_system
|
spark ignition
|
|
gptkbp:maintenance
|
moderate
|
|
gptkbp:manufacturer
|
gptkb:Bristol_Aeroplane_Company
|
|
gptkbp:noise_level
|
moderate
loud
|
|
gptkbp:notable_feature
|
two-row design
|
|
gptkbp:original_run
|
gptkb:1944
|
|
gptkbp:power_output
|
1,600 to 2,000 hp
|
|
gptkbp:production_years
|
1944-1960
|
|
gptkbp:successor
|
gptkb:Bristol_Centaurus
|
|
gptkbp:torque
|
1,500 lb-ft
|
|
gptkbp:tuning
|
supercharged
|
|
gptkbp:type
|
gptkb:radial_engine
|
|
gptkbp:used_in
|
gptkb:Bristol_Freighter
gptkb:Bristol_Beaufighter
gptkb:Bristol_170
gptkb:Avro_Shackleton
|
|
gptkbp:valve_configuration
|
pushrod
|
|
gptkbp:weight
|
1,200 lb
|
|
gptkbp:bfsParent
|
gptkb:Bristol_Beaufighter
gptkb:Short_Stirling
|
|
gptkbp:bfsLayer
|
4
|