Statements (27)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:jet_engine
|
| gptkbp:application |
gptkb:military_aircraft
|
| gptkbp:bore |
150 mm
|
| gptkbp:compression_ratio |
6.5:1
|
| gptkbp:configuration |
liquid-cooled
|
| gptkbp:cooling_system |
liquid cooling
|
| gptkbp:country_of_origin |
gptkb:Soviet_Union
|
| gptkbp:displacement |
27.0 L
|
| gptkbp:engine_configuration |
V-type
|
| gptkbp:engine_type |
reciprocating engine
|
| gptkbp:first_flight |
gptkb:1940
|
| gptkbp:fuel_type |
aviation gasoline
|
| https://www.w3.org/2000/01/rdf-schema#label |
Klimov VK-5 engine
|
| gptkbp:intended_use |
gptkb:fighter_aircraft
|
| gptkbp:manufacturer |
Klimov
|
| gptkbp:number_of_engines |
gptkb:12
|
| gptkbp:power_output |
1,100 hp
|
| gptkbp:production_years |
1940-1945
|
| gptkbp:replaced_by |
gptkb:Klimov_VK-107_engine
|
| gptkbp:stroke |
150 mm
|
| gptkbp:successor |
gptkb:Klimov_VK-107
|
| gptkbp:type |
V-12 engine
|
| gptkbp:used_in |
gptkb:Mikoyan-Gurevich_Mi_G-3
|
| gptkbp:valve_configuration |
overhead valves
|
| gptkbp:weight |
450 kg
|
| gptkbp:bfsParent |
gptkb:Klimov_design_bureau
|
| gptkbp:bfsLayer |
7
|