FORCETALLY
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At a glance
Measured figures
Length
Single source9.75 m (384 in)[source]
Jericho I
Single sourceConfiguration
| Specification | Abdali-I | Jericho (missile) |
|---|---|---|
| Speed | — | Hypersonic[source] |
| Type | SRBM[source] | Ballistic missile[source] |
| Place of origin | Pakistan[source] | Israel[source] |
| Used by | Pakistan Army Army Strategic Forces Command[source] | Israel Defense Forces[source] |
Jericho II
Single sourceJericho III
Single source13.4 m (Jericho I) 14.0 m (Jericho II) 15.5 m (Jericho III)[source]
Maximum; Maximum firing range
Single source450 km (280 mi)[source]
Operational; (as Jericho II) or 4,500-7800 (as Shavit) Up to
Single sourceOperational; Jericho I
Single sourceOperational; Jericho III
Single source500-660 km (Jericho I) 2,800 km (as Jericho II) or 4,500-7800 (as Shavit) Up to 11,500 km (Jericho III)[source]
Warhead weight
Single source500 kg (1,100 lb)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Designer |
|---|
SUPARCO (Rocket stage) DESTO (Warhead design/assembly)[source] |
Initially in collaboration with Dassault Aviation[source] |
| Designed | 1993–97[source] | — |
|---|
| Manufacturer | SUPARCO[source] | Israel Aerospace Industries[source] |
|---|
| Warhead | Single conventional HE / ICM[source] | 400 kg to 1,300 kg warheads[source] |
|---|
| Transmission | Automatic[source] | — |
|---|
| Suspension | MAZ-7310 8WD (With Pakistani military markings)[source] | — |
|---|
| Propellant | Solid-propellent[source] | Solid[source] |
|---|
| Guidance system | Inertial , Terminal[source] | Inertial with terminal guidance[source] |
|---|
| Accuracy | 100 m (330 ft)—150 m (490 ft) CEP .[source] | — |
|---|
| Launch platform | Transporter erector launcher (TEL)[source] | Silo or Mobile (truck-mounted)[source] |
|---|
| In service | — | 1971–1990s (Jericho I) 1989–present (Jericho II) 2011–present (Jericho III)[source] |
|---|
| Unit cost | — | Classified[source] |
|---|
| Produced | — | 1965 onwards (Jericho I) 1980s onwards (Jericho II) 2000s onwards (Jericho III)[source] |
|---|
| No. built | — | Classified[source] |
|---|
| Detonation mechanism | — | Impact and proximity[source] |
|---|
| Engine | — | Multiple-stage solid rocket[source] |
|---|