Properties (49)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
aircraft engine
|
| gptkbp:aircraft |
gptkb:Boeing_B-17_Flying_Fortress
gptkb:Martin_B-26_Marauder gptkb:North_American_B-25_Mitchell gptkb:Lockheed_P-38_Lightning Douglas A-20 Havoc |
| gptkbp:application |
bombers
transport aircraft fighters |
| gptkbp:compressionRatio |
6.5:1
|
| gptkbp:coolingSystem |
air-cooled
direct air cooling |
| gptkbp:cylinderCount |
9
cylindrical |
| gptkbp:displacement |
1,600 cubic inches
|
| gptkbp:engine |
horizontally opposed
aircraft propulsion influenced future engine designs |
| gptkbp:engineConfiguration |
produced in large numbers
single-row radial |
| gptkbp:firstFlight |
1939
|
| gptkbp:fuelType |
aviation gasoline
|
| https://www.w3.org/2000/01/rdf-schema#label |
Wright R-1600 family
|
| gptkbp:is_used_in |
military aircraft
civilian aircraft |
| gptkbp:manufacturer |
gptkb:Wright_Aeronautical_Corporation
|
| gptkbp:notable_feature |
R-1600-1
R-1600-3 R-1600-7 |
| gptkbp:operationalHistory |
gptkb:Korean_War
gptkb:Vietnam_War gptkb:World_War_II |
| gptkbp:performances |
smooth operation
high reliability high power-to-weight ratio versatile applications low vibration robust construction good fuel efficiency moderate maintenance requirements good torque characteristics good throttle response high_altitude_performance |
| gptkbp:powerOutput |
1,600 to 1,800 horsepower
|
| gptkbp:propulsion |
variable-pitch propeller
|
| gptkbp:replacedBy |
gptkb:Wright_R-1820
|
| gptkbp:successor |
gptkb:Wright_R-2600
|
| gptkbp:type |
radial engine
|
| gptkbp:weight |
approximately 800 pounds
|