Hercules engine

GPTKB entity

Statements (54)
Predicate Object
gptkbp:instance_of gptkb:jet_engine
gptkbp:application gptkb:C-130_Hercules
gptkbp:compression_ratio 6.5:1
gptkbp:configuration W-8
gptkbp:control_system mechanical control system
gptkbp:cooling_system air-cooled
gptkbp:displacement 1,200 cubic inches
gptkbp:elevation up to 25,000 feet
gptkbp:emissions_standard low emissions
gptkbp:engine developed in the 1950s
active user community
mass production
four-stroke cycle
extensive support network
comprehensive documentation available
various military applications
ongoing development efforts
legacy in aviation history
innovative technology used
electrical start system
gptkbp:engine_configuration robust design
horizontally opposed
detailed specifications available
cradle-mounted
gptkbp:engine_power high performance
high reliability
popular among military users
gptkbp:engine_type multiple variants available
gptkbp:first_flight gptkb:1954
gptkbp:fuel_capacity 2.5 feet
5.5 feet
gptkbp:fuel_economy moderate
gptkbp:fuel_type aviation gasoline
https://www.w3.org/2000/01/rdf-schema#label Hercules engine
gptkbp:is_tested_for ground testing required
gptkbp:maintenance 1,500 hours
gptkbp:manufacturer gptkb:Hercules_Aerospace
gptkbp:noise_level moderate noise
gptkbp:notable_features high power-to-weight ratio
gptkbp:number_of_engines 8
gptkbp:operational_history used since the 1950s
gptkbp:power_output up to 4,600 horsepower
gptkbp:propeller variable-pitch propeller
gptkbp:propulsion 3,000 pounds
gptkbp:related_to gptkb:Aero-Engine_Corporation
gptkbp:service_ceiling 30,000 feet
gptkbp:successor gptkb:T56_engine
gptkbp:torque wet sump system
gptkbp:training training programs available
gptkbp:type gptkb:turbofan_engine
gptkbp:used_in gptkb:military_aircraft
gptkbp:weight approximately 1,500 pounds
gptkbp:bfsParent gptkb:Nike_Hercules
gptkbp:bfsLayer 6