Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:bfsLayer |
4
|
| gptkbp:bfsParent |
gptkb:Sir_Henry_Royce
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:compression_ratio |
6:1
|
| gptkbp:cooling_system |
liquid-cooled
|
| gptkbp:displacement |
3.5 liters
|
| gptkbp:engine |
gptkb:Rolls-Royce_K_series
horizontally opposed |
| gptkbp:first_introduced |
1930s
|
| gptkbp:fuel_type |
aviation gasoline
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce 210 HP
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce_Limited
|
| gptkbp:notable_users |
gptkb:de_Havilland_DH.89_Dragon_Rapide
|
| gptkbp:powers |
210 horsepower
|
| gptkbp:production_years |
1930s to 1940s
|
| gptkbp:setting |
6-cylinder
|
| gptkbp:successor |
gptkb:Rolls-Royce_250_series
|
| gptkbp:type |
inline engine
|
| gptkbp:used_in |
various aircraft
|
| gptkbp:valve_configuration |
overhead valves
|
| gptkbp:weight |
approximately 150 kg
|