Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:bfsLayer |
7
|
| gptkbp:bfsParent |
gptkb:R-3350-25
|
| gptkbp:compression_ratio |
6.5:1
|
| gptkbp:cooling_system |
Air-cooled
|
| gptkbp:displacement |
3350 cubic inches
|
| gptkbp:engine |
gptkb:battle
|
| gptkbp:first_flight |
1941
|
| gptkbp:fuel_type |
gptkb:Avgas
|
| https://www.w3.org/2000/01/rdf-schema#label |
R-3350-70
|
| gptkbp:manufacturer |
gptkb:Wright_Aeronautical_Corporation
|
| gptkbp:power_output |
2000 to 3500 horsepower
|
| gptkbp:replaced_by |
Turboprop Engines
|
| gptkbp:service_history |
Used in military and civilian aircraft.
|
| gptkbp:setting |
18 cylinders
|
| gptkbp:type |
Radial Engine
|
| gptkbp:used_in |
gptkb:Lockheed_Constellation
gptkb:Douglas_DC-7 |
| gptkbp:valve_configuration |
Pushrod
|
| gptkbp:variant |
gptkb:R-3350-32
R-3350-51 R-3350-23 |
| gptkbp:weight |
approximately 1,800 pounds
|