Press Contacts: Peter Crail, Research Analyst, (202) 463-8270 x102
The Bush administration frequently cites ballistic missiles as one of the leading threats to U.S. security and as a primary rationale for building missile defenses. The following chart lists 32 countries, including the United States and its allies, which currently possess ballistic missiles. For each country, the chart details the type of missile, its operational status, and the best-known public estimates of each missile’s range and payload. The source of the missiles—whether domestically produced, imported, or some combination of the two methods (derived or replicated from foreign technology with or without the original exporter’s consent)—is also provided.
Only nine (China, France, India, Israel, North Korea, Pakistan, Russia, the United Kingdom, and the United States) of the 32 states below are known or suspected of possessing nuclear weapons. These nine states and Iran have produced or flight-tested missiles with ranges exceeding 1,000 kilometers. China and Russia are the only two states that have a proven capability to launch ballistic missiles from their territories that can strike the continental United States.
Ballistic Missile Basics
Ballistic missiles are powered by rockets initially but then they follow an unpowered, free-falling trajectory toward their targets. They are classified by the maximum distance that they can travel, which is a function of how powerful the missile’s engines (rockets) are and the weight of the missile’s payload. To add more distance to a missile’s range, rockets are stacked on top of each other in a configuration referred to as staging. There are four general classifications of ballistic missiles:
- Short-range ballistic missiles, traveling less than 1,000 kilometers (approximately 620 miles);
- Medium-range ballistic missiles, traveling between 1,000–3,000 kilometers (approximately 620-1,860 miles);
- Intermediate-range ballistic missiles, traveling between 3,000–5,500 kilometers (approximately 1,860-3,410 miles); and
- Intercontinental ballistic missiles (ICBMs), traveling more than 5,500 kilometers.
Short- and medium-range ballistic missiles are referred to as theater ballistic missiles, whereas ICBMs or long-range ballistic missiles are described as strategic ballistic missiles. Missiles are often classified by fuel-type: liquid or solid propellants. Missiles with solid fuel require less maintenance and preparation time than missiles with liquid fuel because solid-propellants have the fuel and oxidizer together, whereas liquid-fueled missiles must keep the two separated until right before deployment.
Country |
System[1] |
Status |
Range/Payload[2] |
Source[3] |
---|---|---|---|---|
Afghanistan |
Scud-B |
Unknown[4] |
300 km/1,000kg |
USSR |
Armenia |
Scud-B |
Operational |
300 km/1,000 kg |
Russia[5] |
Bahrain |
ATACMS (MGM-140) |
Operational |
165 km/560 kg |
USA |
Belarus
|
SS-21 |
Operational |
120 km/480 kg |
USSR
|
Scud-B
|
Operational
|
300 km/1,000 kg
|
USSR
|
|
China |
M-7 (CSS-8) |
Operational |
150-230 km/190 kg |
Domestic Production |
DF-3A (CSS-2)
|
Operational
|
2,800 km/2,150 kg
|
Domestic/Russia
|
|
DF-4 (CSS-3)
|
Operational
|
5,470+ km/2,200 kg
|
Domestic Production
|
|
DF-5 (CSS-4, Mod 1)
|
Operational
|
12,000 km/3,200 kg
|
Domestic Production
|
|
DF-5A (CSS-4, Mod 2)
|
Operational
|
13,000 km/3,200 kg
|
Domestic Production
|
|
DF-11 (CSS-7)
|
Operational
|
300 km/500 kg
|
Domestic Production
|
|
DF-15 (CSS-6)
|
Operational
|
600 km/500 kg
|
Domestic Production
|
|
DF-21 (CSS-5, Mod 1)
|
Operational
|
2,500 km/600 kg
|
Domestic Production
|
|
DF-21A (CSS-5, Mod 2)
|
Operational
|
1,770+ km/2,000 kg
|
Domestic Production
|
|
DF-31 (CSS-9)
|
Operational[6]
|
7,250+ km/700 kg
|
Domestic Production
|
|
DF-31A
|
Operational
|
11,270+ km/800 kg
|
Domestic Production
|
|
Julang 1 (SLBM)
|
Operational
|
1,700+ km/600 kg
|
Domestic Production
|
|
Julang 2 (SLBM)
|
Tested/Development
|
8,000 km/700 kg
|
Domestic Production
|
|
Egypt |
Scud-B
|
Operational
|
300 km/1,000 kg
|
USSR/North Korea
|
Project-T (Scud B)
|
Operational
|
450 km/985 kg
|
Domestic/North Korea
|
|
Scud-C
|
Operational
|
550 km/600 kg
|
Domestic/North Korea
|
|
France
|
M4A/B (SLBM)
|
Operational
|
6,000 km/1,200 kg
|
Domestic Production
|
M45 (SLBM)
|
Operational
|
6,000 km/1,000 kg
|
Domestic Production
|
|
M51 (SLBM)
|
Tested/Development
|
8,000 km/1380 kg
|
Domestic Production
|
|
Georgia |
Scud B |
Operational |
300 km/1,000 kg |
USSR |
Greece |
ATACMS (MGM-140) |
Operational |
165 km/560 kg |
USA |
India[7] |
Prithvi-1
|
Operational
|
150 km/1,000 kg
|
Domestic/USSR
|
Prithvi-2
|
Operational
|
250 km/500 kg
|
Domestic/USSR
|
|
Prithvi-3
|
Development
|
350 km/500-1,000 kg
|
Domestic/USSR
|
|
Dhanush
|
Tested/Development
|
250 km/500 kg
|
Domestic Production
|
|
Sagarika (SLBM)
|
Development
|
250-350 km/500 kg
|
Domestic/Russia
|
|
Agni-1
|
Development
|
700 km/1,000 kg
|
Domestic/US/France
|
|
Agni-1 variant
|
Tested/Development
|
1,000 km/1,000 kg
|
Domestic/US/France
|
|
Agni-2
|
Operational
|
2,000 km/1,000 kg
|
Domestic Production
|
|
Agni-3
|
Operational Tested/Development[8]
|
3,000 km/1,000? kg
|
Domestic/Russia
|
|
Surya
|
Development
|
5,500+ km/2,000 kg
|
Domestic
|
|
Iran[9] |
Mushak-120
|
Operational
|
130 km/190 kg
|
Domestic Production
|
Mushak-160
|
Operational
|
160 km/190 kg
|
Domestic Production
|
|
Fateh-110
|
Operational
|
200 km/600 kg
|
Domestic/China
|
|
Tondar-69 (CSS-8)
|
Operational
|
150 km/190 kg
|
China
|
|
Scud-B
|
Operational
|
300 km/1,000 kg
|
Domestic/Libya/North Korea
|
|
Scud-C
|
Operational
|
550 km/600 kg
|
Domestic/North Korea
|
|
Shahab-3
|
Operational
|
1,300-2,000? km/750 kg
|
Domestic/North Korea/Russia
|
|
Shahab-3 variant/Ghadr?
|
Tested/Development?
|
1,800 km/750 kg
|
Domestic/North Korea/Russia
|
|
Shahab-4
|
Development?
|
2,000+ km/1,000 kg
|
Domestic/North Korea/Russia
|
|
Iraq[10] |
Al Fat’h
|
Unknown
|
160 km/200-300 kg
|
Domestic Production
|
Al Samoud II
|
Unknown
|
180-200 km/300 kg
|
Domestic Production
|
|
Israel |
Lance
|
Operational
|
130 km/450 kg
|
USA
|
Jericho-1
|
Operational
|
500 km/750-1,000 kg
|
Domestic/France
|
|
Jericho-2
|
Operational
|
1,500 km/1,000 kg
|
Domestic/France
|
|
Jericho-3
|
Operational?
|
3,000-6,500 km/1,000 kg
|
Domestic Production
|
|
Kazakhstan |
Tochka-U (SS-21)
|
Operational
|
120 km/480 kg
|
USSR
|
Scud-B
|
Operational
|
300 km/1,000 kg
|
USSR
|
|
Libya[11] |
Al Fatah
|
Tested/Development
|
200 km/500 kg
|
Domestic Production
|
Scud-B
|
Operational
|
300 km/1,000 kg
|
USSR
|
|
North Korea |
SS-21 variant
|
Tested/Development
|
100-120 km/ ? kg
|
Domestic/USSR
|
Scud-B
|
Operational
|
300 km/1,000 kg
|
USSR/Egypt?
|
|
Scud-C variant
|
Operational
|
500 km/700 kg
|
Domestic Production
|
|
No-Dong-1
|
Operational
|
1,300 km/700-1,000 kg
|
Domestic Production
|
|
No-Dong-2
|
Tested/Development
|
1,500 km/770 kg
|
Domestic Production
|
|
Taepo Dong-1[12]
|
Tested/Development
|
2,000 km/1,000 kg
|
Domestic Production
|
|
Taepo Dong-2[13]
|
Tested/Development
|
3,500-5,500 km/1,000 kg
|
Domestic Production
|
|
SS-N-6 variant[14]
|
Development
|
2,500-4,000? km/680 kg
|
Domestic Production
|
|
Pakistan |
Hatf-1
|
Operational
|
80-100 km/500 kg
|
Domestic Production
|
Hatf-2
|
Tested/Development
|
190 km/500 kg
|
Domestic/China
|
|
Hatf-3 (Ghaznavi)
|
Operational
|
300 km/500 kg
|
Domestic Production
|
|
Shaheen-1
|
Operational
|
750 km/500 kg
|
Domestic/China
|
|
Ghauri-1
|
Operational
|
1,300 km/700 kg
|
Domestic/North Korea
|
|
Ghauri-2
|
Tested/Development
|
2,300 km/700 kg
|
Domestic/North Korea
|
|
Shaheen-2
|
Tested/Development
|
2,500 km/1,000 kg
|
Domestic/China
|
|
Ghauri-3
|
Development
|
3,000 km/? kg
|
Domestic/North Korea
|
|
Romania |
Scud-B |
Operational |
300 km/1,000 kg |
USSR |
Russia |
Scud-B (SS-1c Mod 1)
|
Operational
|
300 km/1,000 kg
|
Domestic Production
|
Scud-B (SS-1c Mod 2)
|
Operational
|
240 km/950 kg
|
Domestic Production
|
|
SS-18
|
Operational
|
10,000 km/8,800 kg
|
Domestic Production
|
|
SS-19
|
Operational
|
10,000 km/4,350 kg
|
Domestic Production
|
|
SS-21
|
Operational
|
120 km/480 kg
|
Domestic Production
|
|
SS-24
|
Retired
|
10,000 km/4,050 kg
|
Domestic Production
|
|
SS-25
|
Operational
|
10,500 km/1,000 kg
|
Domestic Production
|
|
SS-27 (Topol M)[15]
|
Operational
|
10,500 km/1,000-1,200 kg
|
Domestic Production
|
|
SS-26 (Iskander)
|
Operational
|
400 km/480 kg
|
Domestic Production
|
|
SS-N-8 (SLBM)
|
Operational
|
8,000 km/1,100 kg
|
Domestic Production
|
|
SS-N-18 (SLBM)
|
Operational
|
6,500-8,000 km/1,650 kg
|
Domestic Production
|
|
SS-N-20 (SLBM)
|
Being Retired
|
8,300 km/2,550 kg
|
Domestic Production
|
|
SS-N-23 (SLBM)
|
Operational
|
8,000 km/2,800 kg
|
Domestic Production
|
|
RSM-56 (Bulava-30)
|
Tested/Development
|
10,000 km/1,000-2,000 kg
|
Domestic Production
|
|
Iskander-E
|
Operational
|
280 km/480 kg
|
Domestic Production
|
|
Saudi Arabia |
Dong Feng-3 (CSS-2) |
Operational |
2,600 km/2,150 kg |
China |
Slovakia |
SS-21 |
Operational |
120 km/480 kg |
USSR |
South Korea |
NHK-1
|
Operational
|
180 km/560 kg
|
Domestic/USA
|
NHK-2
|
Operational
|
260-300 km/500 kg
|
Domestic/USA
|
|
ATACMS Block 1/A
|
Operational
|
300 km/560 kg
|
USA
|
|
Syria |
SS-21
|
Operational
|
120 km/480 kg
|
USSR
|
Scud-B
|
Operational
|
300 km/1,000 kg
|
Domestic/USSR
|
|
Scud-C
|
Operational
|
500 km/600-770 kg
|
Domestic/North Korea
|
|
Scud-D
|
Tested/Development
|
700 km/500 kg
|
Domestic/North Korea
|
|
Taiwan |
Ching Feng
|
Operational
|
130 km/270 kg
|
Domestic/Israel
|
Tien Chi
|
Operational
|
300 km/500 kg
|
Domestic Production
|
|
Turkey |
ATACMS (MGM-140)
|
Operational
|
165 km/560 kg
|
USA
|
Project J
|
Development
|
150 km/150 kg
|
Domestic/China
|
|
Turkmenistan |
Scud-B |
Operational |
300 km/1,000 kg |
USSR |
Ukraine |
SS-21
|
Operational
|
120 km/480 kg
|
USSR
|
Scud-B
|
Operational
|
300 km/1,000 kg
|
USSR
|
|
United Arab Emirates |
Scud-B
|
Operational |
300 km/1,000 kg |
USSR |
United Kingdom |
D-5 Trident II (SLBM) |
Operational |
7,400 km/2,800 kg |
USA |
United States |
ATACMS Block I
|
Operational
|
165 km/560 kg
|
Domestic Production
|
ATACMS Block IA
|
Operational
|
300 km/160 kg
|
Domestic Production
|
|
ATACMS Block II
|
Operational
|
140 km/270 kg
|
Domestic Production
|
|
Minuteman III
|
Operational
|
9,650-13,000 km/1,150 kg
|
Domestic Production
|
|
D-5 Trident II (SLBM)
|
Operational
|
7,400+ km/2,800 kg
|
Domestic Production
|
|
Vietnam |
Scud-B |
Operational |
300 km/1,000 kg |
Domestic Production |
Yemen[16] |
Scud-B
|
Operational
|
300 km/1,000 kg
|
USSR
|
SS-21
|
Operational
|
120 km/480 kg
|
USSR
|
|
Scud variant
|
Operational
|
300-500 km/600-1,000 kg
|
North Korea
|
ENDNOTES:
1. All missiles are surface-to-surface unless otherwise noted. SLBM is an acronym for a submarine-launched ballistic missile.
2. The ranges and payloads, given in kilometers (km) and kilograms (kg), respectively, are estimates based on unclassified sources. These figures, however, do not reflect either the missile’s maximum range or its heaviest payload. Equipping a missile with a lighter payload would increase its range. Similarly, a heavier payload would diminish a missile’s range.
3. Several states formerly part of or allied with the Soviet Union retain Soviet SS-21 and Scud missiles. Additionally, according to the Central Intelligence Agency (CIA), continued Russian, Chinese, and North Korean technological and material support remains critical to further development of other foreign missile programs, particularly those of Iran and Pakistan. In its latest version of an annual proliferation report (covering 2004), the CIA noted that ballistic missile assistance from “entities in China, North Korea, and Russia over the years has helped Iran move toward its goal of becoming self-sufficient in the production of ballistic missiles.” In 2004, China announced its interest in joining the voluntary Missile Technology Control Regime (MTCR) but so far has been denied membership because some existing members, including the United States, remain concerned about Chinese missile proliferation.
4. A January 15, 2001 report by the UN Monitoring Group on Afghanistan concluded that prior to the October 2001 U.S.-led offensive in Afghanistan there were approximately 100 Scud-B missiles and at least four Scud mobile launchers in Afghanistan. The current distribution and operational capability of the missiles are unknown, although the UN Monitoring Group speculated that up to 30 of the missiles might be under control of the Northern Alliance.
5. According to a 1997 report by Lev Rokhlin, then-Chairman of the Russian State Duma’s Committee on Defense, Russia transferred eight Scud-B ballistic missiles and 24 Scud launchers, along with other military hardware, to Armenia between 1993-1996. Responding to publication of the report in the Russian newspaper Nezavisimaya Gazeta and to formal requests by the Azerbaijan government, then-Russian President Boris Yeltsin ordered an investigation into the claims. They were subsequently confirmed in April 1997 by Aman Tuleyev, then-Russian minister for relations with the Commonwealth of Independent States.
6. In the Department of Defense’s 2007 report on Chinese military power, the DF-31 ICBM is listed as having “initial threat capability,” meaning it “could be employed in actual military operations” even though it is not yet officially deployed.
7. India and Pakistan claim that their missiles are not deployed, meaning that the missiles are not on launchers, aimed at particular locations, or kept on a high state of alert. The missiles are in a state of “induction” with the nuclear warheads stored in facilities separate from the missile units and airfields. Pakistan and India, however, have deployed their missiles on a number of occasions, such as the Kargil crisis in July 1999.
8. The Agni-3’s first flight test failed on July 9, 2006. The missile dropped into the sea after five minutes of flight. The Indian government declared the missile’s second flight test on April 12, 2007 a success.
9. A great deal of speculation has surrounded Iran’s missile program concerning the possible development of a longer-ranged Shahab-4 and a rumored Shahab-5, supposedly based on the Russian SS-4 and the North Korean Taepo Dong-1, respectively. Iran has denied this assertion, claiming that it has “no plans to develop long-range missiles…since the U.S. is not one of Iran’s strategic defense targets.” A 2005 Congressional Research Service report suggests that perhaps Iran is developing longer-range missiles under the less politically-precarious title of an “improved” or “upgraded” Shahab-3. There also is speculation that Iran has imported a North Korean missile modeled on the Soviet SS-N-6 SLBM. (See endnote 14.)
10. Because of lack of current documentary evidence and inconsistencies in source reporting, the status of Iraq’s ballistic missile arsenal is unclear. The United Nations Monitoring, Verification and Inspection Commission (UNMOVIC) determined in 2003 that the Al Samoud II and the Al Fat’h missiles exceeded the range permitted under UN Security Council Resolution 687. That resolution prohibited Iraq from possessing missiles with ranges exceeding 150 kilometers. UN inspectors began the destruction of these missiles on March 1, 2003, but the inspectors were withdrawn before all of the missiles had been eliminated. According to UNMOVIC’s 13th Quarterly Report, only two-thirds of the Al Samoud II missiles declared by Iraq had been destroyed. The 2004 Iraq Survey Group Report by the United States asserted that a “full accounting of the Al Fat’h missiles may not be possible.”
11. According to a CIA Report, Libya privately pledged to the United States in 2003 that it would eliminate all missiles classified as Category I systems by the MTCR. Category I pertains to missiles capable of traveling 300 kilometers or more with a payload of at least 500 kilograms, the presumed minimum weight for a first-generation nuclear warhead. Libya, however, still maintains a missile development program for systems that fall below the Category I threshold capability.
12. The Taepo Dong-I was first flight-tested August 31, 1998. Its first two stages worked but a third stage failed. The missile has not been flight-tested again.
13. The Taepo Dong-II failed about 40 seconds into its inaugural flight test on July 5, 2006. It has not been flight-tested again.
14. Although North Korea has never flight-tested the SS-N-6 variant, Washington alleges that Pyongyang has deployed the missile. The SS-N-6 originally was a Soviet submarine-launched ballistic missile, but North Korea is reportedly deploying it as a road-mobile missile. There also is speculation that North Korea has transferred this missile to Iran. (See Paul Kerr, “Iran, North Korea Deepen Missile Cooperation,” Arms Control Today, January/February 2007, p. 38.)
16. On December 9, 2002, Spanish forces intercepted a North Korean cargo ship bearing 15 Scud missiles to Yemen. The United States intervened to permit the transfer to be completed because Yemen is considered an important ally in the U.S.-led “War on Terror.” Yemen pledged to cease further arms purchases from North Korea.
Sources: Arms Control Association; Missile Defense Agency; U.S. Department of Defense; Andrew Feickert, Missile Survey: Ballistic and Cruise Missiles of Selected Foreign Countries, Congressional Research Service, July 26, 2005, 39 pp;National Air and Space Intelligence Center, Ballistic and Cruise Missile Threat, March 2006, 29 pp; Office of the Director of National Intelligence, Unclassified Report to Congress on the Acquisition of Technology Relating to Weapons of Mass Destruction and Advanced Conventional Munitions, 1 January 2004-31 December 2004, 10 pp; and Office of the Secretary of Defense, Military Power of the People’s Republic of China 2007, May 25, 2007, 42 pp.
-Researched by Abby Doll