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BBallistic missiles
At a glance
Measured figures
Jericho I
Single sourceJericho II
Single sourceConfiguration
| Specification | Jericho (missile) | Rampage (missile) |
|---|---|---|
| Type | Ballistic missile[source] | — |
| Place of origin | Israel[source] | Israel[source] |
| In service | 1971–1990s (Jericho I) 1989–present (Jericho II) 2011–present (Jericho III)[source] | — |
| Used by | Israel Defense Forces[source] | Israeli Air Force Indian Air Force Indian Navy[source] |
| Designer | Initially in collaboration with Dassault Aviation |
Jericho III
Single source13.4 m (Jericho I) 14.0 m (Jericho II) 15.5 m (Jericho III)[source]
Length
Single source4.7 m (15 ft)[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]
Operational; Operational range
Single source150–250 km (93–155 mi)[source]
Warhead weight
Single source150 kg (330 lb)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Elbit Systems , Israel Aerospace Industries[source] |
| Manufacturer | Israel Aerospace Industries[source] | תעש מערכות ו אלביט מערכות מפעל מלמ של התעשייה האווירית[source]Named manufacturer organization |
|---|
| Unit cost | Classified[source] | — |
|---|
| Produced | 1965 onwards (Jericho I) 1980s onwards (Jericho II) 2000s onwards (Jericho III)[source] | — |
|---|
| No. built | Classified[source] | — |
|---|
| Warhead | 400 kg to 1,300 kg warheads[source] | Multi- EFP[source] |
|---|
| Detonation mechanism | Impact and proximity[source] | Radio proximity fuze , Blast fragmentation[source] |
|---|
| Engine | Multiple-stage solid rocket[source] | Solid-propellant rocket[source] |
|---|
| Propellant | Solid[source] | Solid fuel[source] |
|---|
| Guidance system | Inertial with terminal guidance[source] | INS + Altimeter + GPS + Two-way Datalink[source] |
|---|
| Launch platform | Silo or Mobile (truck-mounted)[source] | F-16 , F-15 , F/A-18E/F , Eurofighter Typhoon , IAI Kfir , Sukhoi Su-30MKI , SEPECAT Jaguar , MiG-29K[source] |
|---|
| Flight altitude | — | 3,000–40,000 ft (910–12,190 m)[source] |
|---|
| Accuracy | — | 10m CEP[source] |
|---|