Jericho (missile)

Jericho
TypeBallistic missile
Place of originIsrael
Service history
In service
  • 1971–1990s (Jericho I)
  • 1989–Present (Jericho II)
  • 2011–Present (Jericho III)
Used by
Production history
DesignerInitially in collaboration with Dassault Aviation
ManufacturerIsrael Aerospace Industries
Unit costClassified
Produced
  • 1965 onwards (Jericho I)
  • 1980s onwards (Jericho II)
  • 2000s onwards (Jericho III)
No. builtClassified
Specifications
Mass
  • 6,500 kg (Jericho I)
  • 26,000 kg (Jericho II)
  • 30,000 kg (Jericho III)
Length
  • 13.4 m (Jericho I)
  • 14.0 m (Jericho II)
  • 15.5 m (Jericho III)
Diameter
  • 0.8 m (Jericho I)
  • 1.56 m (Jericho II and III)
Warhead
  • 400 kg to 1,300 kg warheads
Detonation
mechanism
Impact and proximity

EngineMultiple-stage solid rocket
PropellantSolid
Operational
range
  • 500 km (Jericho I)
  • 1,500 km (Jericho II)
  • Up to 6,500 km (Jericho III)
Maximum speed Hypersonic
Guidance
system
Inertial with terminal guidance
Launch
platform
Silo or Mobile (truck-mounted)

Jericho (Hebrew: יריחו, romanizedYericho) is a general designation given to a loosely-related family of deployed ballistic missiles developed by Israel since the 1960s. The name is taken from the first development contract for the Jericho I signed between Israel and Dassault in 1963, with the codename as a reference to the Biblical city of Jericho. As with some other Israeli high tech weapons systems, exact details are classified, though there are observed test data, public statements by government officials, and details in open literature especially about the Shavit satellite launch vehicle.

The later Jericho family development is related to the Shavit and Shavit II space launch vehicles believed to be derivatives of the Jericho II IRBM and that preceded the development of the Jericho III ICBM.[1] The Lawrence Livermore National Laboratory in the US concluded that the Shavit could be adapted as an ICBM carrying a 500 kg warhead over 7,500 km.[2] Additional insight into the Jericho program was revealed by the South African series of missiles, of which the RSA-3 are believed to be licensed copies of the Jericho II/Shavit, and the RSA-4 that used part of these systems in their stack with a heavy first stage. Subsequent to the declaration and disarming of the South African nuclear program,[3] the RSA series missiles were offered commercially as satellite launch vehicles, resulting in the advertised specifications becoming public knowledge.[4]

The civilian space launch version of the Jericho, the Shavit, was studied in an air launched version piggybacked on a Boeing 747 similar to a U.S. experimental launch of the Minuteman ICBM from a C-5 Galaxy.[5]

  1. ^ "Delivery systems", Israel (country profile), NTI, archived from the original on 2013-09-21, retrieved 2013-06-23.
  2. ^ https://unoda-web.s3-accelerate.amazonaws.com/wp-content/uploads/assets/HomePage/ODAPublications/DisarmamentStudySeries/PDF/SS-23.pdf [bare URL PDF]
  3. ^ Von Wielligh, N. & von Wielligh-Steyn, L. (2015). The Bomb: South Africa’s Nuclear Weapons Programme. Pretoria: Litera.
  4. ^ "RSA-3". Archived from the original on August 20, 2016. Retrieved 7 September 2016.
  5. ^ "Israel Studies Airborne Launch Scheme for Shavit Rocket". SpaceNews.com. Retrieved 6 February 2015.

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