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
|