Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:turbofan_engine
|
| gptkbp:application |
gptkb:military_aircraft
|
| gptkbp:compression_ratio |
16:1
|
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:development |
derived from VK-2500 engine
|
| gptkbp:diameter |
0.5 m
|
| gptkbp:emissions_standard |
gptkb:Euro_I
|
| gptkbp:engine_configuration |
twin-shaft
|
| gptkbp:first_flight |
gptkb:2000
|
| gptkbp:fuel_type |
gptkb:Jet_A-1
|
| https://www.w3.org/2000/01/rdf-schema#label |
VK-2500 V
|
| gptkbp:length |
1.5 m
|
| gptkbp:manufacturer |
Klimov
|
| gptkbp:notable_features |
digital control system
|
| gptkbp:power_output |
2400 hp
|
| gptkbp:propulsion |
2400 lbf
|
| gptkbp:status |
in production
|
| gptkbp:type |
turbo-shaft
|
| gptkbp:used_in |
gptkb:Kamov_Ka-52
gptkb:Mil_Mi-28 |
| gptkbp:weight |
300 kg
|
| gptkbp:bfsParent |
gptkb:VK-2500_engine
|
| gptkbp:bfsLayer |
8
|