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At a glance
Shahab-2larger figure on 0 of 3
Shaheen-IIIlarger figure on 3 of 3
Counts only measures both sources give with the same scope. A larger figure is not a better system.
Measured figures
Mass
Single source6,370–6,500 kg[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Configuration
| Specification | Shahab-2 | Shaheen-III |
|---|---|---|
| Type | Tactical SRBM[source] | MRBM[source] |
| In service | 1990–2016 (in Iran); present (in Syria)[source] | 2015–present[source] |
| Used by | See § Operators[source] | Pakistan Army ( Army Strategic Forces Command )[source] |
| Manufacturer | Iran[source] | National Engineering & Scientific Commission[source] |
| Warhead | 770kg[source] | HE / NE[source] |
| Engine | Liquid[source] | Multi-stage[source] |
| Guidance system | inertial[source] | Inertial , Terminal ,[source] |
| Accuracy | 500m CEP[source] | — |
| Role | tactical short-range ballistic missile[source] | — |
| Source measurement | On November 2, 2006, Iran fired unarmed missiles to begin 10 days of military simulations . Iranian state television reported "dozens of missiles were fired, including Shahab-2 and Shahab-3 missiles. The missiles ranged from 300 km to up to 2,000 km. Iranian experts have made some changes to Shahab-3 missiles, installing cluster warheads in them with the capacity to carry 1,400 bombs."[source]Shahab-2 · History; only the objects and conditions stated in this passage | — |
| Country of origin | Iran[source] Iran[source] | — |
| Place of origin | — | Pakistan[source] |
| Designer | — | National Engineering & Scientific Commission (NESCOM)[source] |
| Designed | — | 2003–2013[source] |
| Variants | — | Ababeel[source] |
| Blast yield | — | >50 kilotons of TNT (210 TJ)[source] |
| Transmission | — | Automatic[source] |
| Suspension | — | WS21200 16WD (with Pakistani military markings)[source] |
| Propellant | — | Solid-fuel[source] |
| Launch platform | — | Transporter erector launcher (TEL), launch pad[source] |
| Reported operators |
| — |