Statements (20)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:bfsLayer |
5
|
| gptkbp:bfsParent |
gptkb:Beriev_A-50
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:design |
A. A. Mikulin
|
| gptkbp:diameter |
1,000 mm
|
| gptkbp:engine |
axial flow
|
| gptkbp:engine_type |
2
8 |
| gptkbp:fuel_type |
kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
Ilyushin AL-21 F-3
|
| gptkbp:length |
4,200 mm
|
| gptkbp:manufacturer |
gptkb:Ilyushin
|
| gptkbp:origin |
gptkb:Monarch
|
| gptkbp:original_run |
gptkb:1955
|
| gptkbp:propulsion |
11,000 lbf
|
| gptkbp:replaced_by |
AL-21 F-3 M
|
| gptkbp:type |
turbojet
|
| gptkbp:used_in |
gptkb:Ilyushin_Il-28
|
| gptkbp:weight |
1,200 kg
|