Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:diameter |
0.9 m
|
| gptkbp:engine |
turbojet
annular |
| gptkbp:engine_type |
axial
single-stage |
| gptkbp:fuel_type |
kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
Klimov VK-30
|
| gptkbp:length |
3.5 m
|
| gptkbp:manufacturer |
Klimov
|
| gptkbp:origin |
gptkb:Monarch
|
| gptkbp:original_run |
1950
|
| gptkbp:propulsion |
3000 lbf
|
| gptkbp:successor |
gptkb:Klimov_VK-1
|
| gptkbp:type |
gptkb:engine
|
| gptkbp:used_in |
gptkb:Mikoyan-Gurevich_Mi_G-17
gptkb:Mikoyan-Gurevich_Mi_G-15 gptkb:Mikoyan-Gurevich_Mi_G-19 |
| gptkbp:weight |
400 kg
|
| gptkbp:bfsParent |
gptkb:Klimov_VK-28_engine
|
| gptkbp:bfsLayer |
8
|