Statements (29)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:bfsLayer |
6
|
| gptkbp:bfsParent |
gptkb:Continental_A-65
|
| gptkbp:application |
gptkb:Taylorcraft_BC-12_D
gptkb:Cessna_140 gptkb:Piper_J-3_Cub |
| gptkbp:bore |
3.125 inches
|
| gptkbp:compression_ratio |
6.5:1
|
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:displacement |
75 cubic inches
|
| gptkbp:engine |
gptkb:V8
8 V engine |
| gptkbp:first_introduced |
1940s
|
| gptkbp:fuel_type |
aviation gasoline
carbureted |
| https://www.w3.org/2000/01/rdf-schema#label |
Continental A-75
|
| gptkbp:ignition_system |
magneto
|
| gptkbp:manufacturer |
gptkb:Continental_Motors
|
| gptkbp:power_output |
75 horsepower
|
| gptkbp:production_years |
1940s to 1950s
|
| gptkbp:propulsion |
fixed-pitch
|
| gptkbp:setting |
air-cooled
|
| gptkbp:stroke |
3.0 inches
|
| gptkbp:successor |
gptkb:Continental_O-200
|
| gptkbp:type |
gptkb:engine
|
| gptkbp:used_in |
gptkb:aircraft
|
| gptkbp:valve_configuration |
overhead valve
|
| gptkbp:weight |
approximately 200 pounds
|