R-36 (missile)

R-36; NATO reporting name: SS-18 Satan
Type	Intercontinental ballistic missile
Place of origin	USSR
Service history
In service	1967 - Present
Used by	Soviet and Russian Strategic Rocket Forces
Production history
Manufacturer	Yuzhny Machine-Building Plant
Specifications
Weight	209,600 kg (462,000 lb)
Length	32.2 m (106 ft)
Diameter	3.05 m (10.0 ft)
Warhead	Three stage fission-fusion-fission, over 20 Mt of TNT
Detonation mechanism	Airburst
Engine	Two-stage liquid propellant
Operational range	10,200–16,000 km (depending on R-36M missile variants)
Speed	up to 7.9 km/s
Guidance system	Inertial, autonomous
Accuracy	220–700 m CEP (depending on R-36M missile variants)
Launch platform	Silo

The R-36, (Russian: Р-36) is a family of intercontinental ballistic missiles (ICBMs) and space launch vehicles designed by the Soviet Union during the Cold War. The original R-36 was produced under the Soviet industry designation 8K67 and was given the NATO reporting name SS-9 Scarp. The later version, the R-36M was produced under the GRAU designations 15A14 and 15A18 and was given the NATO reporting name SS-18 Satan. This missile was viewed by certain U.S. analysts as giving the Soviet Union first strike advantage over the U.S., particularly because of its very heavy throw weight and extremely large number of re-entry vehicles. Some versions of the R-36M were deployed with 10 warheads and up to 40 penetration aids and the missile's high throw-weight made it theoretically capable of carrying more warheads or penetration aids. Contemporary U.S. missiles, such as the Minuteman III, carried up to three warheads at most.

Contents 1 Description 2 R-36M (SS-18) variants 2.1 Deployed variants of R-36M missiles[2][3] 3 Development 4 Multiple warheads 5 Deployment 6 R-36ORB 7 Elimination 8 Derivatives 9 Operators 10 See also 11 References 12 External links

Description

The R-36 (SS-9) is a two-stage rocket powered by a liquid bipropellant, with UDMH as fuel and nitrogen tetroxide as an oxidizer. It carries one of three types of re-entry vehicles (RVs) developed especially for this missile:

• The Mod 1 and Mod 2 carried single nuclear warheads of 18 and 25 megatons (mt) of TNT yield respectively.
• The Mod 4 carried three multiple independently targeted re-entry vehicles (MIRV).

An additional version, the Mod 3, was proposed (it was to be a Fractional Orbital Bombardment System (FOBS), a missile that travels through space in a low-earth orbit), but was not adopted due to the Outer Space Treaty.

The R-36P missile was developed to carry the Mod 4 warhead, while the R-36O (the letter O) was to be for the Mod 3 FOBS. R-36 and R-36P missiles were hot launched from their silos.

The R-36M (SS-18) is similar to the R-36 in design, but has the capacity to mount a MIRV payload of 10 warheads, each with a 550–750 kt yield, or a single warhead of up to 20 mt. Throw-weight of the missile is 8,800 kg. This makes the Soviet R-36 the world's heaviest ICBM; for comparison, the heaviest US ICBM (the retired LGM-118 Peacekeeper, that carried 10 warheads of 300 kT each) had less than a half of this at 4,000 kg. The R-36M has two stages. The first is a 460,000 kgf (4.5 MN) thrust motor with four combustion chambers and nozzles. The second stage is a single-chamber 77,000 kgf (755 kN) thrust motor.

R-36M (SS-18) variants

• R-36M (SS-18 Mod 1): The SS-18 Mod 1 carried a single large reentry vehicle, with a warhead yield of 18-25 MT, a distance of about 6000 nm. In January 1971, cold-launch tests began during which the mortar launch was perfected. The actual flight tests for the single-RV Mod 1 began on 21 February 1973, though some sources suggest that testing began in October 1972. The testing phase of the R-36M with various different types of warheads was finished in October 1975 and on 30 December 1975 deployment began (though some Western sources suggest that an initial operational capability was reached in early 1975). A total of 56 were deployed by 1977, though all were replaced by Mod 3 or Mod 4 missiles by 1984. These high-yield weapons were assessed in the West as possibly developed to attack American Minuteman ICBM launch control centers. Tom Clancy described this potential tasking as the ability to 'turn Cheyenne Mountain into Cheyenne Lake.'^[1]

• R-36M (SS-18 Mod 2): The SS-18 Mod 2 included a post-boost vehicle and up to eight reentry vehicles, each with a warhead yield estimated at between 0.5 to 1.5 MT, with a range capability of about 5500 nm. The MIRVs were placed in pairs, and a post boost vehicle with a command structure and a propulsion system were contained in the nose cone of the R-36M. The flight tests of the MIRVed Mod 2 began in September 1973 (though some Western sources suggest that the initial flight test of the Mod 2 MIRV version occurred in August 1973), with IOC in 1975. Approximately 132 were deployed by 1978, but the post-boost vehicle design was seriously flawed, and the Mod 2 missiles were all replaced by the Mod 4 variant by 1983.

• R-36M (SS-18 Mod 3): The SS-18 Mod 3 carried a single large reentry vehicle that was an improved version of the SS-18 Mod 1. On 16 August 1976, a few months after the R-36M entered service, the development of an improved modification of the R-36M (15A14) was approved. This missile subsequently received the designation R-36MUTTh (15A18) and was developed by KB Yuzhnoye (OKB-586) through December 1976. The R-36MUTTh was capable of carrying two different nose cones. On 29 November 1979, deployment of the improved R-36M with a single reentry vehicle carrying a 18-25 MT warhead (SS-18 Mod 3) began.

• R-36MUTTh (SS-18 Mod 4): The SS-18 Mod 4 was probably designed to attack and destroy ICBMs and other hardened targets in the US. Its increasing accuracy made it possible to reduce the yield of the warheads and allowed an increase in the number of warheads from 8 to 10. According to some Western estimates, evidence suggested that the Mod 4 may be capable of carrying as many as 14 RVs (this may reflect observation of the deployment of countermeasures intended to overcome a ballistic missile defense, or to confuse American attack characterization systems). The flight-design tests of the R-36MUTTh began on 31 October 1977 and in November 1979 the flight tests of the MIRVed missile were completed. The first three regiments were put on alert on 18 September 1979. During 1980 a total of 120 SS-18 Mod 4 missiles were deployed, replacing the last remaining R-36 (SS-9) missiles. In 1982–1983 the remaining R-36M missiles were also replaced with the new R-36MUTTh and the total number of deployed missiles reached the maximum 308 ceiling established in the SALT-1 treaty. The SS-18 Mod 4 force had the estimated capability to destroy 65 to 80 percent of US ICBM silos using two nuclear warheads against each. Even after this type of attack, it was estimated that more than 1000 SS-18 warheads would be available for further strikes against targets in the US. After 2009, the SS-18 Mod 4s were all eliminated in favor of the newer SS-18 Mod 5.

• R-36M2 Voivode (SS-18 Mod 5): The newer, more accurate SS-18 Mod 5 version placed in converted silos allowed the SS-18 to remain the bulwark of the SRF's hard-target-kill capability. The Mod 5 carries 10 MIRVs, each having a higher yield than the Mod 4 warheads. The Mod 5 warheads have nearly twice the yield of the Mod 4 (approximately 750 KT to 1 MT) according to Western estimates, though Russian sources suggest a yield of 550-750 KT each. The increase in the Mod 5's warhead yield, along with improved accuracy, would, under the START treaty, help allow the Russians to maintain their hard-target-kill wartime requirements even with the 50 percent cut in heavy ICBMs the START agreement required. The technical proposals to build a modernized heavy ICBM were made in June 1979. The missile subsequently received the designation R-36M2 Voivode and the industrial index number 15A18M. The design of the R-36 M2 Voivode was completed in June 1982. The R-36M2 consisted of a series of new engineering features. The engine of the second stage is completely built in the fuel tank (earlier this was only used on SLBMs) and the design of the transport-launching canister was altered. Unlike the R-36M, the 10 warheads on the post-boost vehicle are located on a special frame in two circles. The flight tests of the R-36M2 equipped with 10 MIRVs began in March 1986 and were completed in March 1988. The first regiment with these missiles was put on alert on 30 July 1988 and was deployed on 11 August 1988.

• R-36M2 Voivode (SS-18 Mod 6): The flight tests of the R-36M2 missile carrying a single warhead (SS-18 Mod 6) with a yield of 20 MT were completed in September 1989 and deployment began in August 1991. Ten Mod 6 missiles were deployed. One intended use of these large warheads was high altitude detonation to incapacitate electronics and communications through a very large electromagnetic pulse. The SS-18 Mod 6 missiles were all decommissioned by late 2009.

At full deployment, before the fall of the Soviet Union in 1991, 308 SS-18 launch silos were operational. After the breakup of the USSR, 204 of these were located on the territory of the Russian Federation and 104 on the territory of newly independent Kazakhstan. The dismantling of 104 launchers located in Kazakhstan was completed in September 1996. The START II treaty was to eliminate all SS-18 missiles but it did not enter into force and the missiles remained on duty. Russia has steadily decreased the number of operational SS-18s and by July 2009, only 59 (all of the 10 MIRV Mod 5 version) remain. About 40 missiles will have their service lives extended so that they remain in service until about 2020. With the retirement of the 20 megaton SS-18 Mod 6 warheads, the highest yield weapon in service with any nation is the estimated 5 MT Chinese Dong Feng 5 (DF-5) ICBM (CSS-4) warhead.

All R-36 variants were designed to be launched from silos in dispersed and hardened locations. The R-36M is placed into its 39 m deep silo in a tubular storage/launch container. Upon launch the missile is shot out of the tube, mortar-fashion, by a piston, driven by the expansion of gases from a slow-burning black powder charge inside the piston. The missile's main engine is ignited tens of metres above the ground, preventing any damage to the internal equipment of the silo itself from the rocket engine's fiery efflux.

Deployed variants of R-36M missiles^[2][3]

System:	R-36M	R-36M	R-36M	R-36MUTTH	R-36MUTTH	R-36M2
Treaty-designation:	RS-20A	RS-20A1	RS-20A2	RS-20B	RS-20B	RS-20V
GRAU-designation:	15A14	15A14	15A14	15A18	15A18	15A18M
NATO-designation:	SS-18 Satan Mod 1	SS-18 Satan Mod 2	SS-18 Satan Mod 3	SS-18 Satan Mod 4	SS-18 Satan Mod 5	SS-18 Satan Mod 6
Deployment:	1974–1983	1976–1980	1976–1986	1979–2005	1986–2009	1988–Present
Maximum deployed number:	148	10	30	278	30	58
Length:	32.6 m	32.6 m	32.6 m	36.3 m	36.3 m	34.3 m
Diameter:	3.00 m	3.00 m	3.00 m	3.00 m	3.00 m	3.00 m
Launch weight:	209,600 kg	209,600 kg	210,000 kg	211,100 kg	211,100 kg	211,100 kg
Number of warheads:	8	10	1	10	1	10
Warhead yield:	4 x 1.0 MT + 4 x 0.4 MT	0.4 MT	20 MT	0.5 MT	20 MT	0.8 MT
Range:	11,200 km	10,200 km	16,000 km	11,000 km	16,000 km	11,000 km
CEP:	700 m	700 m	700 m	370 m	370 m	220 m

Development

Development of the R-36 was begun by OKB-586 (Yuzhnoye) in Dnipropetrovsk, Ukraine in 1962, and built upon the work of the R-16 program. The Chief Designer was Mikhail Yangel. Initial development was of light, heavy, and orbital versions, with flight testing from 1962 through 1966, at which time initial operational capability was achieved. News of the development of the orbital version caused alarm in the West with the possibility that the Soviets would be able to launch a large number of nuclear weapons into orbit where there was no capability to intercept them. The prospect of orbital nuclear weapons led both sides to agree a treaty banning the use of weapons of mass destruction in space.

In 1970, development of a fourth version, capable of delivering multiple warheads, was developed, and test flown the next year.

Further improvement of the R-36 led to the design of the R-36M, which provided a theoretical first-strike capability—the ability to destroy the United States' LGM-30 Minuteman ICBM silos and launch control centers before they could retaliate. However, neither the Soviet Union nor the Russian Federation have ever publicly delineated the missile's particular role in their arsenal. The initial design of the R-36M called for a single massive 12-Mt warhead to be delivered over a range of 10,600 km. The missile was first tested in 1973 but this test ended in failure. After several delays the R-36M was deployed in December of 1975. This “Mod-1” design was delivered with a single 18–20 Mt warhead and a range of just over 11,000 km. This new version was given a new identity by NATO: SS-18 Satan.

The SS-18 has gone through six separate modifications, with the first modification (Mod-1) being phased out by 1984. The final modification (Mod-6) designated R-36M-2 “Voevoda” was deployed in August of 1988. This missile could deliver the same 18–20 Mt warhead 16,000 km. Modifications prior to Mod-6 mainly introduced MIRV (Multiple independent reentry vehicles) warheads. These missiles (Mods-2, 4, and 5) surpassed their western counterpart the US LGM-118 Peacekeeper in terms of megatons delivered, range, and survivability, but were inferior in terms of accuracy (CEP).

Control system for this rocket was designed at NPO "Electropribor"^[4] (Kharkiv, Ukraine).

Multiple warheads

Missiles of the R-36M/SS-18 family have never been deployed with more than ten warheads, but given their large throw-weight (8.8 tonnes as specified in START), they have the capacity to carry considerably more detonation power. Among the projects that the Soviet Union considered in the mid-1970s was that of a 15A17 missile—a follow-on to the R-36MUTTH (15A18).^[5] The missile would have had an even greater throw-weight—9.5 tonnes—and would be able to carry a very large number of warheads. Five different versions of the missile were considered. Three of these versions would carry regular warheads—38 × 250 kt yield, 24 × 500 kt yield, or 15–17 × 1 Mt yield. Two modifications were supposed to carry guided warheads (“upravlyaemaya golovnaya chast”)—28 × 250 kt or 19 × 500 kt.^[5] However, none of these upgraded models were ever developed. The SALT II Treaty, signed in 1979, prohibited increasing the number of warheads ICBMs could carry. Equally, from a strategic point of view, concentrating so many warheads on silo-based missiles was not seen as desirable, since it would have made a large proportion of the USSR's warheads vulnerable to a counterforce strike.

The operational deployment of the R36M/SS-18 consisted of the R-36MUTTH, which carried ten 500 kt warheads, and its follow-on, the R-36M2 (15A18M), which carried ten 800 kt warheads (single-warhead versions with either 8.3 Mt or 20 Mt warhead also existed at some point). To partially circumvent the treaty, the missile was equipped with 40 heavy decoys to utilize the capacity left unused due to the 10-warhead limitation,.^[6] These decoys would appear as warheads to any defensive system, making each missile as hard to intercept as 50 single warheads, rendering potential anti-ballistic defense ineffective.

Deployment

At full deployment, before the fall of the Soviet Union in 1991, 308 R-36M launch silos were operational. After the breakup of the USSR, 204 of these were located on the territory of the Russian Federation and 104 on the territory of newly independent Kazakhstan. Part of the missiles in Kazakhstan (54 of them) were under the 57th Rocket Division at Zhangiz-Tobe (Solnechnyy), Semipalatinsk Oblast.^[7] The other R-36 establishment in Kazakhstan was the 38th Rocket Division at Derzhavinsk, Turgay Oblast.^[8] In the next few years Russia reduced the number of R-36M launch silos to 154 to conform with the START I treaty. The missiles in Kazakhstan were all deactivated by 1995. The subsequent START II treaty was to eliminate all R-36M missiles but it did not enter into force and the missiles remained on duty.

R-36ORB

The development of the R-36 missile complex for use with the 8К69 fractional-orbit missile ("FOBS") began on April 16, 1962. Such a missile provides some advantages over a conventional ICBM. The range is limited only by the parameters of the orbit that the re-entry vehicle has been placed into, and the re-entry vehicle may come from either direction, compelling the enemy to build considerably more expensive anti-missile systems. Due to the possibility of placing the warhead in orbit and keeping it there for some time, it is possible to reduce the time required to strike to just a few minutes. It is also much more difficult to predict where the warhead will land, since while the re-entry vehicle is on orbit, it is a very small object with few distinguishing marks and is hard to detect; moreover, since the warhead can be commanded to land anywhere along the orbit's ground track, even detecting the warhead on orbit does not allow accurate prediction of its intended target.

The structure and design of the fractional-orbit bombardment system were similar to a conventional P-36 ICBM system. A two-stage rocket was equipped by the liquid rocket engines using storable propellants. The silo launcher and command point were hardened against a nuclear explosion. The basic difference from a conventional ICBM consists of the design of the re-entry vehicle, which is fitted with a single 2.4Mt warhead, de-orbit engine and control block. The control system uses independent inertial navigation and radar-based altimeter which measures orbit parameters twice—in the beginning of an orbital path and just before de-orbiting engine firing.

Flight testing consisted of 15 successful launches and four failures. During test launch #17, the warhead was retrieved with a parachute. Flight tests of a rocket have been completed by May 20, 1968 and on November 19 of the same year it entered service. The first (and the only) regiment with 18 launchers was deployed on August 25, 1969.

The R-36orbs (8К69) were retired from service in January, 1983 as a part of SALT II treaty (they were considered "space-based" nuclear weapons).

The Tsyklon series of civilian space launchers is based on the R-36orb (8К69) design.

Elimination

In the last decade Russian armed forces have been steadily reducing the number of R-36M missiles in service, withdrawing those that age past their designed operational lifetime. About 40 missiles of the most modern variant R-36M2 (or RS-20V) will remain in service until 2019^[9] and will be then replaced by newer MIRV version of Topol-M.^[10] In March 2006 Russia made an agreement with Ukraine that will regulate cooperation between the two countries on maintaining the R-36M2 missiles. It was reported that the cooperation with Ukraine will allow Russia to extend the service life of the R-36M2 missiles by at least ten to 28 years.^[11]

In December 2008 Strategic Rocket Forces had 75 R-36MUTTH/R-36M2 operational missiles.

The commander of the Strategic Rocket Forces Lt. Gen. Andrei Shvaichenko announced on December 16, 2009, that Russia planned to "develop a new liquid-propellant ICBM to replace the Voyevoda (SS-18 Satan), capable of carrying 10 warheads, by 2016."^[12]

Derivatives

Several remaining SS-18 missiles have been modified for surface launch and now carry lightweight satellites to Low Earth Orbit (LEO), including many foreign payloads.

Operators

 Soviet Union and  Russia

The Strategic Rocket Forces have been the only operator of the R-36.

57th Rocket Division at Zhangiz-Tobe (Solnechnyy), Semipalatinsk Oblast;

38th Rocket Division at Derzhavinsk, Turgay Oblast

other Rocket Divisions

See also

• List of missiles
• List of military rockets

References

• Podvig, Pavel (2001). Russian Strategic Nuclear Forces. Cambridge, MA: The MIT Press.

External links

• [1]
• [2]
• [3]
• [4]
• Russia's nuclear forces - 2006, The Bulletin of the Atomic Scientists, March/April 2006
• Yuzhnoe Design Bureau—English-language home page
• Strategic Rocket Forces—Russian strategic nuclear forces
• R-36—Federation of American Scientists
• Strategic Missile Forces museum (photos)

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