Jump to content

Jericho (missile)

From Wikipedia, the free encyclopedia

This is an old revision of this page, as edited by 79.180.126.207 (talk) at 08:09, 20 September 2015 (→Jericho II: link 'islamist revolution' to Iranian Revolution, clarify that previous regime was the Shah's). The present address (URL) is a permanent link to this revision, which may differ significantly from the current revision.

Jericho is a general designation given to the Israeli ballistic missiles. 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 is true for most Israeli unconventional weapons systems, exact details are highly classified though there is 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 which preceded the development of the Jericho III ICBM.[1] Additional insight into the Jericho program is given by the South African series of missiles which the RSA-3 are believed to be licensed copies of the Jericho II/Shavit and the RSA-4 used part of these systems in their stack with a heavy first stage, after the declaration and disarming of the South African nuclear program the RSA series missiles were offered commercially as satellite launch vehicles where the advertised specifications became part of the public knowledge.[2] The civilian space launch version of the Jericho, the Shavit has been studied in an air launched version piggybacked on a Boeing 747 similar to a US experimental launch of the Minuteman ICBM from a C-5 Galaxy.[3]

Jericho I

Jericho I was first publicly identified as an operational short-range ballistic missile system in late 1971. It was 13.4 metres (44 ft) long, 0.8 m (2 ft 7 in) in diameter, weighing 6.5 tonnes (14,000 lb). It had a range of 500 km (310 mi) and a CEP of 1,000 m (3,300 ft), and it could carry a payload estimated at 400 kilograms (880 lb). It was intended to carry a nuclear warhead.[4][5] However, due to Israel's ambiguity over its nuclear weapons program, the missile is classified as a ballistic missile. Initial development was in conjunction with France, Dassault provided various missile systems from 1963 and a type designated MD-620 was test fired in 1965. But French co-operation was halted by an arms embargo from January 1968, though 12 missiles had been delivered from France.[5] Work was continued by IAI at the Beit Zachariah facility and the program cost almost $1 billion up to 1980, incorporating some US technology.[6] Despite some initial problems with its guidance systems, it is believed that around 100 missiles of this type were produced.

In 1969 Israel agreed with the U.S. that Jericho missiles would not be used as "strategic missiles", with nuclear warheads, until at least 1972.[7] The Jericho I is now considered obsolete and was taken out of service during the 1990s.

Jericho II

File:Shavit-1.jpg
Shavit launch

The Jericho II is a solid fuel, two-stage long-range ballistic missile system and a follow on from the Jericho I project.

A request from Israel for 1,100 mile (1,770 km) range Pershing II medium range ballistic missiles was rejected by the US for inclusion as part of a military assistance incentive package offered in 1975 during negotiations over transferring the Sinai from Israeli to Egyptian control as part of a US brokered peace deal.[8] Jericho II development began in 1977, and by 1986 there were reports of test firings. According to Missilethreat, a project of the George C. Marshall Institute, there is evidence the Jericho II originated as a joint Israeli-Iranian project; cooperation which ended with the loss of friendly relations after the 1979 Islamist revolution overthrew the Shah's rule.[9] There was a series of test launches into the Mediterranean from 1987 to 1992, the longest at around 1,300 km, mostly from the facility at Palmachim, south of Tel Aviv. Jane's reports that a test launch of 1,400 km is believed to have taken place from South Africa's Overberg Test Range in June 1989.[10]

The Jericho II is 14.0 m long and 1.56 m wide, with a reported launch weight of 26,000 kg (although an alternative launch weight of 21,935 kg has been suggested). It has a 1,000 kg payload, capable of carrying a considerable amount of high explosives or a 1 Mt yield nuclear warhead. It uses a two-stage solid propellant engine with a separating warhead. The missile can be launched from a silo, a railroad flat truck, or a mobile vehicle. This gives it the ability to be hidden, moved quickly, or kept in a hardened silo, largely ensuring survival against any attack.[11]

The Jericho II forms the basis of the three-stage, 23 ton Shavit NEXT satellite launcher, first launched in 1988 from Palmachim. From the performance of Shavit it has been estimated that as a ballistic missile it has a maximum range of about 7,800 km with a 500 kg payload.[6]

The Jericho II as an available Israeli counter attack option to Iraqi missile bombardment in the 1991 Gulf War is disputed. Jane's at the time believed that Jericho II entered service in 1989.[12] Researcher Seth Carus claims that according to an Israeli source the decision to operationally deploy the Jericho-2 was only made after 1994 several years after the Scud attacks had ended and a cease fire and disarmament regime were in place. [13] Raytheon quoting Soviet intelligence archives showing them believing the Jericho-2 as an fully developed weapon in 1989, but did not indicate when it was available for deployment. [14] Investigators for the Carnegie Endowment for International Peace accessed commercial satellite images of the Sdot Micha Airbase near Zachariah, a suspected Jericho missile base, comparison shows expansion between 1989 and 1993 of the type which would accommodate suspected Jericho II launchers and missiles. [15] Such an expansion would be more consistent with a post-1991 deployment chronology.

South African RSA Series

The Jericho II/Shavit SLV was also license produced in the Republic of South Africa as the RSA series of space launch vehicles and ballistic missiles.

The RSA-3 was produced by the Houwteq (a discontinued division of Denel) company at Grabouw, 30 km east of Cape Town. Test launches were made from Overberg Test Range near Bredasdorp, 200 km east of Cape Town. Rooi Els was where the engine test facilities were located. Development continued even after South African renunciation[16] of its nuclear weapons for use as a commercial satellite launcher. Development actually reached its height in 1992 a year after nuclear renunciation with 50 - 70 companies involved, employing 1300 -1500 people from the public and private sector.[17][18] A much heavier ICBM or space launch vehicle, the RSA-4, with a first stage in the Peacekeeper ICBM class but with Jericho-2/RSA-3 upper stage components was in development,[19] the RSA-2 was a local copy of the Jericho II ballistic missile and the RSA-1 was a local copy of the Jericho II second stage for use as a mobile missile.[2][20][21][22]

The missiles were to be based on the RSA-3 and RSA-4 launchers that had already been built and tested for the South African space programme. According to Al J Venter author of How South Africa built six atom bombs these missiles were incompatible with the available large South African nuclear warheads, he claims that the RSA series being designed for a 340 kg payload would suggest a warhead of some 200 kg, “well beyond SA's best efforts of the late 1980s.” Venter's analysis is that the RSA series was intended to display a credible delivery system combined with a separate nuclear test in a final diplomatic appeal to the world powers in an emergency even though they were never intended to be used in a weaponized system together.[23] Three rockets had already been launched into suborbital trajectories in the late 1980s in support of development of the RSA-3 launched Greensat Orbital Management System (for commercial satellite applications of vehicle tracking and regional planning). Following the decision in 1989 to cancel the nuclear weapons program, the missile programs were allowed to continue until 1992, when military funding ended, and all ballistic missile work was stopped by mid-1993. In order to join the Missile Technology Control Regime the government had to allow American supervision of the destruction of key facilities applicable to both the long range missile and the space launch programmes.[24]

Variant Date of Launch Launch Location Payload Mission Status
RSA-3 1989 June 1 Overberg Test Range South Africa RSA-3-d 1 Apogee: 100 km (60 mi)
RSA-3 1989 July 6 Overberg Test Range South Africa RSA-3 2 Apogee: 300 km (180 mi)
RSA-3 1990 November 19 Overberg Test Range South Africa RSA-3 3 Apogee: 300 km (180 mi)

In June 1994 the RSA-3 / RSA-4 South African satellite launcher program was cancelled[25]

Jericho III

It is believed that that the Jericho III is a nuclear armed ICBM which entered service in 2008. The Jericho III is believed to have a three-stage solid propellant and a payload of 1,000 to 1,300 kg. It is possible for the missile to be equipped with a single 750 kg nuclear warhead or two or three low yield MIRV warheads. It has an estimated launch weight of 30,000 kg and a length of 15.5 m with a width of 1.56 m. It may be similar to an upgraded and re-designed Shavit space launch vehicle, produced by Israel Aerospace Industries. It probably has longer first and second-stage motors. It is estimated by missilethreat.com that it has a range of 4,800 to 6,500 km (2,982 to 4,038 miles),[26] though USAF missile proliferation survey for the Congressional Research Service puts possible maximum range at 11,500 km.[27]

According to an official report which was submitted to the American congress in 2004, it may be that with a payload of 1,000 kg the Jericho III gives Israel nuclear strike capabilities within the entire Middle East, Africa, Europe, Asia and almost all parts of North America, as well as within large parts of South America and North Oceania. Missile Threat reports: "The range of the Jericho 3 also provides an extremely high impact speed for nearby targets, enabling it to avoid any Anti-Ballistic Missile (ABM) defenses that may develop in the immediate region."[26] On 17 January 2008 Israel test fired a multi-stage ballistic missile believed to be of the Jericho III type, reportedly capable of carrying "conventional or non conventional warheads."[28] On 2 November 2011, Israel successfully test fired a missile believed to be an upgraded version of the Jericho III at Palmachim; the long trail of smoke was seen throughout central Israel.[29] Israel's intercontinental ballistic missile launchers are believed to be buried so far underground that they would survive a nuclear attack.[30][31]

After a further test in 2013 Alon Ben David published this opinion in an article in Aviation Week on the missile's range and throw weight "Reportedly, Israel's Jericho III intermediate-range ballistic missile is capable of carrying a 1,000-kg (2,204-lb.) warhead more than 5,000 km."[32]

See also

References

  1. ^ "Delivery systems", Israel (country profile), NTI.
  2. ^ a b "RSA-3". Retrieved 6 February 2015.
  3. ^ "Israel Studies Airborne Launch Scheme for Shavit Rocket". SpaceNews.com. Retrieved 6 February 2015.
  4. ^ Prospects for Further Proliferation of Nuclear Weapons (PDF), Special National Intelligence Assessment, CIA, 23 August 1974, SNIE 4-1-74, retrieved 2008-01-20
  5. ^ a b Kissinger, Henry A (16 July 1969), "Israeli Nuclear Program" (PDF), Memorandum for the President, The White House, retrieved 2009-07-26
  6. ^ a b "Ballistic Missile Proliferation". Canadian Security Intelligence Service. March 23, 2001. 2000/09. Retrieved 2010-06-21.
  7. ^ Kissinger, Henry A (7 October 1969), "Discussions with the Israelis on nuclear matters" (PDF), Memorandum for the President, The White House, retrieved 2006-07-02
  8. ^ "Missiles for Peace". Time. September 29, 1975. Archived from the original (PDF) on February 2, 2008.
  9. ^ http://missilethreat.com/missiles/jericho-123/
  10. ^ "Shavit (Israel), Space launch vehicles – Orbital". Jane's Information Group. 2009-04-21. Retrieved 2010-04-17.
  11. ^ "Jericho 2". MissileThreat. 2008-01-17. Retrieved 2010-06-21.
  12. ^ Duncan Lennox, ed., "Jericho 1/2/3 (YA-1/YA-3) (Israel), Offensive Weapons," Jane's Strategic Weapon Systems, Issue 50, (Surrey: Jane's Information Group, January 2009), pp. 84-86.
  13. ^ Seth W. Carus, "Israeli Ballistic Missile Developments," Testimony before the Commission to Assess the Ballistic Missile Threat to the United States, 15 July 1998, www.fas.org.
  14. ^ Raytheon Systems Company, Missile Systems of the World, (Bremerton, WA: AMI International, 1999), p. 459.
  15. ^ Joseph Cirincione, Jon B. Wolfsthal and Miriam Rajkumar, Deadly Arsenals: Tracking Weapons of Mass Destruction (Washington, DC, Carnegie Endowment for International Peace, 2002), p. 230. Identifying the specific deployment date of the Jericho-2 arsenal at Sdot Micha would provide knowledge about the operational status of the Jericho-2 during the 1991 Iraq War. Probable test flights from Israel and South Africa around 1989 would indicate that the R&D phase of the Jericho-2 project was nearing completion at that date. However, scale-up and transition from the R&D phase to the manufacturing phase would likely have required several years, as would necessary expansion or modifications to the Sdot Micha airbase. Commercial satellite images showing expansion of the base would be consistent with a deployment date roughly 4 to 5 years after the initial test flights, thus implying that the Jericho-2 was not yet deployed during the 1991 Iraq War.
  16. ^ http://www.armscontrol.org/system/files/ACT_South%20Africa_9601.pdf
  17. ^ Iain McFadyen. "The South African Rocket & Space Programme". Retrieved 6 February 2015.
  18. ^ Guy Martin. "Satellites for South Africa". Retrieved 6 February 2015.
  19. ^ "RSA-4". Retrieved 6 February 2015.
  20. ^ "RSA". Retrieved 6 February 2015.
  21. ^ "RSA-1". Retrieved 6 February 2015.
  22. ^ "RSA-2". Retrieved 6 February 2015.
  23. ^ Leon Engelbrecht. "Book Review: How SA built six atom bombs". Retrieved 6 February 2015.
  24. ^ "Jericho". Archived from the original on 29 May 2010. Retrieved 6 February 2015.
  25. ^ "South Africa". Retrieved 6 February 2015.
  26. ^ a b "Jericho 3". Missile Threat. 2012-03-26. Retrieved 2012-09-12.
  27. ^ http://www.au.af.mil/au/awc/awcgate/crs/rl30427.pdf
  28. ^ Azoulay, Yuval (18 January 2008). "Missile test 'will improve deterrence'". Haaretz. Retrieved 5 January 2012.
  29. ^ Pfeffer, Anshel (2 November 2011). "IDF test-fires ballistic missile in central Israel". Haaretz. Retrieved 3 November 2011.
  30. ^ Plushnick-Masti, Ramit (2006-08-25). "Israel Buys 2 Nuclear-Capable Submarines". The Washington Post. Retrieved 2010-05-20.
  31. ^ Missile survey: ballistic & cruise missiles of foreign countries (PDF).
  32. ^ "Israel Tests Enhanced Ballistic Missile". Retrieved 6 February 2015.
Retrieved from "https://en.wikipedia.org/w/index.php?title=Jericho_(missile)&oldid=681901951"