Statements (25)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:radial_engine
|
| gptkbp:application |
bombers
|
| gptkbp:compression_ratio |
6:1
|
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:design_date |
1930s
|
| gptkbp:displacement |
28 liters
|
| gptkbp:engine |
gptkb:W-18_engine
|
| gptkbp:engine_configuration |
horizontally opposed
|
| gptkbp:first_flight |
1940s
|
| gptkbp:fuel_type |
aviation gasoline
|
| https://www.w3.org/2000/01/rdf-schema#label |
W-28 radial engine
|
| gptkbp:ignition_system |
magneto ignition
|
| gptkbp:manufacturer |
gptkb:Wright_Aeronautical_Corporation
|
| gptkbp:number_of_engines |
gptkb:28
radial |
| gptkbp:operational_use |
gptkb:World_War_II
|
| gptkbp:power_output |
1,000 hp
|
| gptkbp:propeller |
variable pitch
|
| gptkbp:successor |
gptkb:W-34_radial_engine
|
| gptkbp:type |
gptkb:jet_engine
|
| gptkbp:used_in |
gptkb:military_aircraft
|
| gptkbp:valve_configuration |
overhead valves
|
| gptkbp:weight |
1,200 lbs
|
| gptkbp:bfsParent |
gptkb:Pratt_&_Whitney_R-4360
|
| gptkbp:bfsLayer |
6
|