Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:surface-to-air_missile
|
| gptkbp:diameter |
400 mm
|
| gptkbp:elevation |
22 km
|
| gptkbp:engineType |
piston engine
|
| gptkbp:enteredService |
1983
|
| gptkbp:guidanceSystem |
semi-active radar homing
|
| https://www.w3.org/2000/01/rdf-schema#label |
9M38
|
| gptkbp:length |
5.55 m
|
| gptkbp:manufacturer |
gptkb:Dolgoprudny_Research_Production_Enterprise
|
| gptkbp:origin |
gptkb:Soviet_Union
|
| gptkbp:range |
35 km
|
| gptkbp:speed |
Mach 3
|
| gptkbp:successor |
gptkb:9M38M1
|
| gptkbp:usedBy |
gptkb:Finland
gptkb:India gptkb:Russia gptkb:Ukraine |
| gptkbp:usedIn |
gptkb:Buk_missile_system
|
| gptkbp:warheadType |
70 kg
high-explosive fragmentation |
| gptkbp:weight |
685 kg
|
| gptkbp:bfsParent |
gptkb:Buk_missile_system
|
| gptkbp:bfsLayer |
6
|