Statements (25)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:surface-to-air_missile
|
| gptkbp:basedOn |
North Korean Nodong-1
|
| gptkbp:countryOfOrigin |
gptkb:Iran
|
| gptkbp:diameter |
1.32 m
|
| gptkbp:engine |
single-stage liquid-fueled
|
| gptkbp:enteredService |
2003
|
| gptkbp:guidanceSystem |
gptkb:GPS
inertial |
| gptkbp:length |
16.58 m
|
| gptkbp:manufacturer |
Aerospace Industries Organization
|
| gptkbp:payload |
760–1,200 kg
|
| gptkbp:platform |
road-mobile transporter erector launcher
|
| gptkbp:propulsion |
gptkb:water
|
| gptkbp:range |
1,000–2,000 km
|
| gptkbp:status |
in service
|
| gptkbp:testLaunches |
since 1998
|
| gptkbp:type |
medium-range ballistic missile
|
| gptkbp:usedBy |
gptkb:Iranian_Army
gptkb:Islamic_Revolutionary_Guard_Corps |
| gptkbp:warheadType |
conventional
potential nuclear |
| gptkbp:weight |
17,400 kg
|
| gptkbp:bfsParent |
gptkb:Safir
|
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Shahab-3 missile
|