Statements (56)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:application |
gptkb:Douglas_DC-3
gptkb:Lockheed_Electra gptkb:Grumman_F4_F_Wildcat gptkb:North_American_T-6_Texan gptkb:Boeing_Stearman_PT-17 |
| gptkbp:compression_ratio |
6.5:1
|
| gptkbp:cooling_system |
air-cooled
direct air cooling |
| gptkbp:displacement |
1340 cubic inches
|
| gptkbp:engine |
gptkb:9
high reliability four-stroke horizontally opposed front-mounted over 30,000 units radial design single-row used in many classic aircraft |
| gptkbp:engine_type |
R-1340-AN-1
R-1340-AN-17 R-1340-AN-3 R-1340-AN-6 R-1340-AN-7 R-1340-AN-10 R-1340-AN-11 R-1340-AN-12 R-1340-AN-13 R-1340-AN-14 R-1340-AN-15 R-1340-AN-16 R-1340-AN-18 R-1340-AN-19 R-1340-AN-2 R-1340-AN-20 R-1340-AN-4 R-1340-AN-5 R-1340-AN-8 R-1340-AN-9 |
| gptkbp:fuel_type |
aviation gasoline
carbureted |
| https://www.w3.org/2000/01/rdf-schema#label |
P& WR-1340 Wasp
|
| gptkbp:ignition_system |
dual ignition
|
| gptkbp:manufacturer |
gptkb:Pratt_&_Whitney
|
| gptkbp:original_run |
1925
|
| gptkbp:power_output |
600 horsepower
|
| gptkbp:propulsion |
variable pitch
|
| gptkbp:setting |
air-cooled
|
| gptkbp:successor |
P& WR-985 Wasp Junior
|
| gptkbp:type |
gptkb:engine
|
| gptkbp:used_in |
gptkb:aircraft
civilian aircraft |
| gptkbp:valve_configuration |
pushrod actuated
|
| gptkbp:weight |
400 pounds
|
| gptkbp:bfsParent |
gptkb:DHC-25_B
|
| gptkbp:bfsLayer |
6
|