No wonder the NATO called her “Satan. No wonder the NATO called her "Satan" The radius of destruction of a nuclear missile satan

The threat of the use of nuclear weapons by a "partner" in " cold war", the creation of an ever-expanding missile defense system, were a challenge that the USSR was obliged to respond to.

In the seventies of the last century, a strategic complex was created, where the main element was the ballistic missile R-36 Satan, classified in NATO SS-18 "Satan".

"Satan" is able to destroy the protected targets of the enemy.

Protected by the missile defense system, including the framework of a retaliatory strike after repeated use nuclear weapons.

Until now foreign designs armaments failed to even come close to the parameters possessed by combat characteristics Satan.

History reference

Survey work on the P-36M Satan was carried out by specialists from the Yuzhnoye Design Bureau (KB) in the city of Dnepropetrovsk. The Ukrainian city has now been renamed Dnipro.

this year, work began on the RS "Satan"

At the same time, the engineers did not upgrade the existing R-36 Voevoda, but applied new solutions that meet the requirements for the security and effectiveness of weapons:

• placement of the launcher and launch control point in premises with maximum protection;
• autonomous missile control system;
• minimum time for pre-launch preparation and launch;
• remote prelaunch programming of targets from the control room;
• increased survivability of all missile system;
• cruising speed of the Satan missile has been increased;
• the ability of the SS-18 to overcome the barriers created by the enemy's missile defense system;
• a start that does not give the possibility of fixing the place of its holding;
• breakthrough in the maximum radius, accuracy of hitting targets;
• resistance to the consequences of close, to the placement of the installation, a nuclear explosion (gamma, beta, x-rays).

The finished product was tested at Baikonur in the winter of 1973. Improvements continued until the fall of 1975, but the need to protect the country from possible aggression forced the R-36M to be put on duty as early as 1974.

In the future, the SS-18 rocket was constantly upgraded. For example, it completed the modification of the carrier and warhead of the missile. After testing in the late seventies, the Satan ballistic missile was replaced by the R36M ICBM.

The performance characteristics of Satan have been finalized and improved, where the control system had better characteristics, the warhead was divided into ten warheads of 0.55 Mt each, with a radius of destruction of up to 300.0 thousand square meters. km, flight speed up to 2.5 km / s, each.

The design of the ballistic missile Satan

The design of the SS-18, including the placement of the main units and assemblies, has the following features:

• two-stage, with separation of stages in sequential order;
• fuel, oxidizer are in adjoining tanks separated by a partition;
• control cables, pneumatic and hydraulic control systems are routed along the body and protected by a special casing;
• the first stage is equipped with four rocket engines, the fuel is supplied in a closed cycle, while the engines are autonomous;
• flight control is carried out by an autonomous control system;
• the second stage is equipped with a sustainer and a four-chamber flight path-controlling rocket engine;
• to improve the protective qualities, when the enemy uses nuclear weapons, where a missile is launched, the body is covered with a special black heat-shielding composition;
• pre-installed sensors monitor the level of aggressive radiation, and if they are present, they turn off all control systems, but when leaving this zone, they conduct automatic switch on, the control system makes adjustments to the trajectory to achieve the set goal of destruction.

The new Satan rocket, whose characteristics have demonstrated high hit accuracy rates, are provided by an inertial control system based on on-board computing equipment, has become the main weapon of the Strategic Missile Forces. The radius of destruction of Satan, which became known in NATO, cooled the hot heads of the hawks.

Satan rocket engine

The rocket engines and fuel supply system were created on the basis of the latest, for that period, developments of the country's advanced design bureaus:

• the use of chemical pressurization of fuel tanks;
• deceleration of the separated stage by pressurization gases;
• equipment of the first and second stages with marching and independent control engines;
• principle of control of divided warheads;
• operation of engines using tetroxide nitrogen fuel and others.

For the first stage, the RD-264 propulsor was used, which was assembled from four elements of the RD-263. The second stage was equipped with a marching propeller RD-0228. All engine samples during testing showed results that excluded malfunctions and failures of control systems.

It should be noted that a new method of launching missiles was introduced, which excludes the fixation of an earth-based missile defense system. The rocket engines were launched at the bottom of the shaft, and due to the accumulation of exhaust gases, at the start, the rocket was “fired” to a considerable height. This made it possible to perceive the launch as a flight of a low-flying aircraft.

Tactical and technical characteristics of the Satan rocket (TTX)

Note: Information obtained from open sources.

The most powerful missile on Earth today is the RS-36M or SS-18 "Satan" (according to the classification of NATO specialists), according to Russian system The designation of the weapon is called "Voevoda". It has been in service with the Strategic Missile Forces since the late 70s to the present day.

This is the most scary rocket for potential enemies, since there is no unattainable point on Earth for it, and in a matter of seconds, its combat charge will sweep away all life within a radius of 500 km2. Therefore, in the West, the RS-36M is considered the creation of the devil. The presence of such weapons prevents aggression from Western "partners" and serves as a deterrent to unleashing a global war.

Story

The two-stage intercontinental ballistic missile "Satan" was developed on the basis of another R-36 missile, but the designers made significant improvements. The design of weapons began in 1969, the assembly of experimental samples was completed by the end of 1975.

In 1970, changes were made to the design to improve the reliability of the main parts and equipment. In the middle of the same year, all regulatory authorities approved the final design of the "Satan" and the Yuzhnoye design bureau received permission to produce the upgraded RS-36M. The last test launches were made at the end of November 1979.

The Satan rocket was created by specialists from the Yuzhnoye design bureau, headed by M.K. Yangel, and after his death - V.F. Utkin. A completely unique intercontinental missile was designed with improved technical parameters.

When launching rockets with a large mass, specialists were faced with the problem of their depreciation in mines.

The designers of the legendary Spetsmash design bureau decided to use compressed gas to give acceleration at the start. A similar principle was called the mortar launch, which was the first time for a weapon of this size and weight. The use of such a scheme significantly reduces the mass of the combat unit and the cost of its launch.

In addition, specialists created shock absorbers that made it possible to launch more massive missiles than the Satan. Thanks to the unique launch method, the RS-36M "Voevoda" is at least 30 years ahead of all the existing missile systems in the world.

Muscovites from KBTM also joined the developers from Yuzhnoye Design Bureau and Spetsmash Design Bureau. Project manager V. Solovyov proposed a pendulum mounting system in the silo. The project was approved by the Ministry of General Machinery and approved for release, but the development of Spetsmash with a mortar launch method using reinforced shock absorbers was adopted in its final form.

The final design of the R-36M included 4 types of warheads:

1. single-block MS 15F171 with BB 15F172 - power more than 20 Mt;
2. MIRV 15F173 includes 10 unguided high-speed warheads (BB) 15F174 - the power of each is more than 0.8 Mt;
3. MS 15F175 with a “light” BB 15F176 - power about 8.3 Mt;
4. split warhead 15F177 with six unguided BB 15F174 and four controlled BB 15F178.

There were other developments, but they did not reach the series.

Installation technology in the mine and testing

In order to carry out full-scale tests of the upgraded missile system in 1971, a special launch pad was created at Baikonur. During the test, a dummy rocket was used, since to test similar weapons without catastrophic consequences for environment impossible.

The testers tested the ability of "Satan" to fly up to at least a height of 20 meters. The performance of the engines and the timeliness of their launch were also checked. A total of 43 launches were made, 36 of which were successful, but 7 times the rocket model fell to the ground.

The designers have provided a revolutionary for our country installation method according to the plant-start scheme. It provided for the complete assembly of Voyevoda at the plant, followed by installation directly into the mine.

As a result, the time spent by the complex without protection was reduced.

The main risk remained only at the stage of delivery of the complex to the launch site. "Satan" was brought by rail, the container was reloaded without using a crane onto a special transport trolley. By means of this trolley, it was delivered to the silo and automatically mounted.

The docking of the rocket itself with its warhead was carried out after it was refueled. To do this, about 180 tons of poisonous and rather aggressive substances were poured into the tanks. After connecting the parts of the rocket, the roof of the silo was closed, sealed and handed over to guard rocketmen.

Design features

Specially for new rocket Design Bureau "Energomash" designed the RD-264 engine, consisting of 4 rocket launchers RD-263 with one chamber. It was installed on the first step of "Satan". The second stage was equipped with a single-chamber sustainer engine RD-0228, created by specialists from the Chemical Automation Design Bureau, headed by A. Konopatov.

Further production was carried out at Yuzhmash, Dnepropetrovsk. Additionally, there is a four-chamber steering engine. Propulsion systems operate on unsymmetrical dimethylhydrazine with nitrogen tetraoxide oxidizer. An intermediate pan separates the fuel tank and the oxidizer tank.

The stages are separated according to the principle of gas dynamics - the explosive bolts connecting the parts of the rocket are triggered, the pressurization gases of the fuel tanks are ejected through the windows intended for this.

A network of cables and a pneumohydraulic system, protected by a casing, are carried along the hull.

The digital computer system installed on board the Satan is responsible for the accuracy of the shooting. Combat equipment is characterized by increased reliability, hit accuracy, nuclear safety during storage, fire safety, resistance to various types radiation.

In the event that potential adversaries use a nuclear strike on the R-36M base area, the heat-shielding coating will help overcome the contaminated zone, and the gamma-neutron sensors will turn off power plant, but the engines will remain operational. The missile will continue to move outside the danger zone and hit the previously planned target. Thus, "Satan" is not vulnerable to the enemy's nuclear forces and systems missile defense.

Design solutions improved such a characteristic as firing accuracy three times compared to the previously created R-36. The launch preparation time was reduced by almost 4 times. Launcher protection has been improved 30 times.

Tactical and technical characteristics

TTHR-36M "Satan" are unique and still have no analogues in the world. The missile has excellent combat and technical specifications. The most significant of them are presented in the table.

Despite repeated attempts by our so-called Western "partners" to destroy or significantly reduce the stock of these missiles in the country's nuclear shield system, "Voivods are still serving on the borders of Russia. They will work for the defense of the country in the Strategic Missile Forces of the Russian Federation until 2026.

Combat use

In service with Russia today are 75 "Satan". The missiles carry 750 nuclear warheads. In total, the nuclear shield of the Russian Federation has more than 1670 warheads, and half of them are "Satan". But since 2015, some of the missiles of this modification have been gradually replaced by more modern combat missile systems.

The combat use of "Satan" has never been carried out due to the fact that it is very powerful deadly weapon can cause irreparable damage to the environment and humanity as a whole. The use of even one missile can lead to the disappearance of, for example, an entire state in the United States. In the mid 80s. the mass replacement of the R-36M with improved installations was carried out.

Instead of recycling because of its high cost, it was decided to use them to launch artificial satellites.

The R-36M is inaccessible to electromagnetic impulses, since the control systems of the "Voevody" are duplicated by pneumatic and electronic machines. To overcome the enemy's missile defense, "Satan" was equipped with decoys, both light and quasi-heavy, dipole reflectors and active jamming generators.

Thanks to the efforts of Soviet scientists and designers who worked on the creation of the Satan or Voyevoda ballistic missile system, the most unique and powerful weapon on the planet was created. These intercontinental missiles are the pride of the Russian Strategic Missile Forces even today.

Despite the enormous efforts made, the potential adversaries of the Russian Federation have so far been unable to create anything of the kind of power and effectiveness. Russia need not be afraid for the security of our Motherland and its inhabitants.

Video

The RS-20V "Voevoda" or R-36M, known as the "Satan" SS-18 (NATO designation) is the most powerful missile in the world. "Satan" will remain in the combat composition of the Russian Strategic Missile Forces until 2026. The heavy missile SS-18 "Satan" is the world's most powerful intercontinental ballistic missile, it was put into service in December 1975, and its first test launch was carried out in February 1973.

R-36M missiles in various modifications can carry from 1 to 10 (in some cases up to 16) warheads with a total mass (with a breeding unit and a nose fairing) up to 8.8 thousand kg for a distance of over 10 thousand km. Two-stage missiles in Russia are placed in highly protected mines, where they are stored in a special transport and launch container that provides them with a "mortar" launch. The strategic missile has a diameter of 3 m and a length of more than 34 m.

Quantity and cost

Missiles of this type are the most powerful of the existing intercontinental missiles, they are capable of inflicting a crushing nuclear strike on the enemy. In the West, these missiles are called "Satan".

The Russian Strategic Missile Forces for 2019 have 75 combat missile systems equipped with Satan missiles (a total of 750 nuclear warheads). This is almost half nuclear capability Russia, with a total of 1677 warheads. By the end of 2019, most likely, another part of the Satan missiles will be removed from Russian service and replaced with more modern missiles.

Tactical and technical characteristics

R-36M "Satan" has the following performance characteristics:

• Number of steps - 2 + dilution block
• Fuel - stored liquid
• Type of launcher - silo with mortar launch
• Power and number of warheads - MIRV 8 × 900 KT, two monoblock options; MIRV 8×550-750 kt
• Head part weight - 8800 kg
• Maximum range with light warhead - 16000 km
• Maximum range with heavy warhead - 11200 km
• Maximum range with MIRV - 10200 km
• Control system - inertial autonomous
• Accuracy - 1000 m
• Length - 36.6 m
• Maximum diameter - 3 m
• Starting weight - 209.6 tons
• Fuel weight - 188 tons
• Oxidizing agent - nitrogen tetroxide
• Fuel - UDMH (heptyl)

History of creation

The R-36M heavy intercontinental ballistic missile was developed at Yuzhnoye Design Bureau (Dnepropetrovsk). On September 2, 1969, a resolution was adopted by the Council of Ministers of the USSR on the creation of the R-36M missile system. The rocket was supposed to have high speed, power and other high performance. The draft design was completed by the designers in December 1969. The intercontinental nuclear ballistic missile provided for 4 types of combat equipment - with multiple, maneuvering and monoblock warheads.

Design Bureau "Yuzhnoye" after the death of the famous M.K. Yangel was headed by Academician V.F. Utkin. When creating a new rocket, which received the designation R-36M, they used all the experience gained by the team when creating previous rocket models. In general, it was new missile system with unique performance characteristics, and not a modification of the R-36. The development of the R-36M went in parallel with the design of other third-generation missiles, common features TTX which were:

• use of MIRV;
• use of an autonomous control system with an onboard computer;
• location of the command post and missiles in high-security structures;
• the possibility of remote re-aiming immediately before launch;
• availability of more advanced means of overcoming missile defense;
• high combat readiness, providing a quick start;
• use of a more advanced management system;
• increased survivability of complexes;
• increased radius of destruction of objects;
• increased combat effectiveness characteristics, which are provided by increased power, speed and accuracy of missiles.
• the radius of the R-36M damage zone by a blocking nuclear explosion is reduced by a factor of 20 compared to the 15A18 missile, resistance to gamma-neutron radiation is increased by 100 times, resistance to X-ray radiation is increased by 10 times.

The intercontinental nuclear ballistic missile R-36M was first launched from the Baikonur test site on February 21, 1973. Tests of the missile system were completed only by October 1975. In 1974, the first missile regiment was deployed in Dombarovsky.

Design features

1. The R-36M is a two-stage rocket that uses sequential stage separation. The fuel and oxidizer tanks are separated by a combined intermediate bottom. Along the body there is an onboard cable network and pipelines of the pneumohydraulic system, which are closed by a casing. The 1st stage engine has 4 autonomous single-chamber liquid-propellant rocket engines, which have a turbo-pump fuel supply in a closed circuit, they are hinged in the tail part of the stage on the frame. The deviation of the engines at the command of the control system allows you to control the flight of the rocket. The 2nd stage engine includes a single-chamber sustainer and a four-chamber steering rocket engine.
2. All engines run on nitrogen tetroxide and UDMH. The R-36M implemented many original technical solutions, for example, chemical pressurization of tanks, deceleration of a separated stage using the expiration of pressurization gases, and the like. The R-36M is equipped with an inertial control system, which operates thanks to the onboard digital computer system. Its use allows for high accuracy of shooting.
3. The designers foresaw the possibility of launching the R-36M2 even after an enemy nuclear strike on the area where the missiles were located. "Satan" has a dark heat-shielding coating that facilitates passage through the radiation dust cloud that appeared after nuclear explosion. Special sensors that measure gamma and neutron radiation during the passage of the nuclear "mushroom" register it and turn off the control system, but the engines continue to work. After leaving the danger zone, the automation turns on the control system and corrects the flight path. ICBMs of this type had a particularly powerful combat equipment. There were two variants of the MS: MIRV with eight BBs (900kt each) and a monoblock thermonuclear (24Mt.). There was also a complex to overcome missile defense systems.

Video of the Satan rocket

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RS-20V, now called "Voevoda" or R-36M, or the ballistic missile SS-18 - "Satan", better known in the world NATO classification. She is the most powerful rocket on the planet. "Satan" still has to be on combat duty in the Russian Strategic Missile Forces.

Ballistic missile SS-18 - Satan"

The missile will remain in combat post for a long time, and 2025 will be the last year for this task. Heavy rocket SS-18 "Satan" is considered the most powerful on the planet. The intercontinental ballistic missile "Satan" was adopted by the Soviet Armed Forces in 1975. The first launch to start in the test mode of the Satan rocket was made in 1973.

Ballistic missile "Satan" SS-18 (R-36M)

The R-36M missile of a wide variety of modifications can carry, together with its launch weight of up to 212 tons, warheads of 1-10, and sometimes up to 16. The total mass, including the breeding unit and the nose fairing, can be more than eight thousand kg and cover a distance of more than ten thousand km. The placement of two-stage missiles in Russia is carried out using highly protected mines.

There they are in special transport and launch containers with the used "mortar" launch. Strategic missiles have a diameter of three meters and a length of up to 35 meters. The missiles have excellent combat and technical characteristics, and they were created in the Dnepropetrovsk NPO Yuzhnoye (now the city of Dnipro) in the 1970s.

Number and price

Each missile of this type is the most powerful in the world. No existing intercontinental missile is capable of inflicting a more devastating nuclear strike on the enemy. It is because of this unprecedented power in the Western media that this rocket was called "Satan". Actually, this power frightened the entire world community. So during the negotiations, which discussed the reduction of offensive weapons. American representatives took a variety of steps to completely reduce them and ban the modernization of these "heavy" weapons.

The Russian Strategic Missile Forces currently have at their disposal more than seventy ballistic missiles equipped with Satan missiles, which have more than 700 nuclear warheads. And this, according to available data, is about half of the entire Russian nuclear shield, which has a total of more than 1670 warheads. Since mid-2015, it was assumed that a certain number of Satan missiles would be removed from the RVSN armament, which they planned to replace with newer missiles.

In 1983, the number of SS-18 launchers in a wide variety of modifications reached 308 units. In 1988, the replacement of early modifications with the R-36M2 began to take place. total strength missiles with launchers were left unchanged, and this was in line with the Soviet-American agreement. The decommissioned Satan missiles were to be disposed of. Nevertheless, recycling at its cost turned out to be quite an expensive exercise. As a result, at the very top they decided to use rockets to launch satellites.

Thus, the Dnepr launch vehicles turned out to be a minor modification of the Russian intercontinental ballistic missiles R-36M. Intercontinental ballistic missiles "Dnepr" at the price of one launch cost no more than 30 million dollars. The payload at this moment is calculated at 3700 kilograms, and this is together with the system for mounting the apparatus.

Thus, the cost of launching a kilogram of payload into orbit is cheaper than using other available launch vehicles. Such relatively inexpensive launches of launch vehicles easily attract customers. However, with a relatively small payload, the missiles also had corresponding limitations. Thus, the launch of the Satan rocket with a launch weight of approximately 210 tons was classified as a light ballistic missile.

Tactical and technical data of the rocket "Satan"

Rocket R-36M "Satan" has:

• Two steps with dilution block;
• liquid fuel;
• The launcher, which is a mine, has a mortar launch;
• Power and number of b / blocks: two monoblock versions; MIRV IN 8×550-750 kt;
• Head part weighing 8800 kg;
• With a light warhead with a maximum range of up to 16,000 km;
• With a heavy warhead with a maximum range of up to 11,200 km;
• With MIRV with a maximum range of up to 10,200 km;
• Inertial autonomous control system;
• Accurate hit within a radius of 1,000 meters;
• More than 36 meters long;
• The largest diameter is up to 3 meters;
• Launch weight up to almost 210 tons;
• Weight of fuel up to 188 tons;
• Oxidizing agent - nitrogen tetroxide;
• Fuel - UDMH;
• Thrust control of the first stage up to 4163/4520 kN;
• The specific impulse of the first stage is up to 2874/3120 m/s.

Some information from the history of the rocket "Satan"

The R-36M heavy-class intercontinental ballistic missile was created in the Dnepropetrovsk Design Bureau "Yuzhnoye" (the current city of Dnipro). Work began in September 1969 after the adoption by the Council of Ministers Soviet Union resolutions on the creation of R-36M missile systems. The missiles were supposed to have high speed, power and other significant characteristics. The completion of the draft design by the designers took place in the winter of 1969. Intercontinental nuclear ballistic missiles were envisaged with four varieties in combat equipment. Separate, maneuvering and monoblock warheads were supposed.

When working on a new missile, which was given the R-36M marking, everything that was the best at that time was used. All the experience accumulated by scientists, which was accumulated during the creation of previous missile systems, was used. As a result, they created a new rocket with rare technical specifications, and not a modification of the R-36. Work on the creation of the R-36M went simultaneously with another project. These were third-generation missiles, their specificity was:

• Use of MIRV;
• The use of autonomous control systems with onboard computers;
• The command post and missile were in a highly secure facility;
• Remote re-aiming must be done before launch;
• More advanced means of overcoming missile defense;
• The presence of high combat readiness, which was provided by a quick start;
• Advanced control system;
• The presence of increased survivability in the complexes;
• Increased radius when hitting objects;
• Increased combat effectiveness, which should provide an increase in the power, speed and accuracy of missiles;
• A twenty-fold reduction in the radius of damage during a blocking nuclear explosion relative to 15A18 missiles, resistance to gamma-neutron radiation increased by 100 times, resistance to X-ray radiation - ten times.

The intercontinental nuclear ballistic missile R-36M was first tested at the famous Baikonur test site in February 1973. The missile system was only completed in October 1975. In order not to be delayed with the deployment, we decided to put him on combat duty. In 1974, the deployment of the first missile regiment took place in the city of Dombarovskoye.

For the first missiles, monoblock warheads were selected, with a capacity of 24 Mt. Since 1975, the regiments received the R-36M with warhead IN with eight BBs, with a capacity of 0.9 Mt each. 1978-1980 - conducting test launches of the R-36M, which have maneuvering warheads, but they were not accepted into service.

Subsequently, the R-36M intercontinental nuclear ballistic missiles were replaced by the R-36M UTTKh ICBMs. They differed in modified aggregate-instrument blocks, and also had a more advanced control system. A significant improvement has also occurred with the operational characteristics of the DBK, as well as with an increase in the security of command posts and silos. Test launches were made in 1977-1979 at Baikonur. Launches were carried out using warheads with 10 BBs, each with a capacity of 0.55 Mt.

Strategic missile systems R-36M UTTKh with 15A18 missiles, which are equipped with 10-block multiple warheads, are universal, highly effective systems strategic purpose. One R-36M UTTKh missile can defeat up to ten targets. It is possible to defeat large and high-strength small-sized area targets in an environment of effective countermeasures against enemy missile defense.

The radius of destruction reaches 300,000 sq. km. When one of the warheads is aimed at the target, its speed near the earth's surface during braking in the atmosphere becomes significantly lower than when approaching the atmospheric area. In particular, the flight speed of the separating warheads at an altitude of 25 km at the end of the AC 4 km/s could be 2.5 km/s. The encounter rates of modern AP ICBMs near surfaces are still classified.

Design features of the rocket "Satan"

The R-36M are two-stage missiles using successive stage separations. The fuel and oxidizer tanks are separated by a combined intermediate bottom. The onboard cable network and pneumohydraulic pipes were laid along the hull and closed with a casing. The first stage engine has four autonomous single-chamber liquid-propellant rocket engines, with an existing turbopump fuel supply in a closed cycle. The missile is controlled in flight by commands from the control system. The engine of the second stage contains the presence of a single-chamber sustainer and a four-chamber steering rocket engine.

The operation of all engines is due to nitrogen tetroxide and UDMH. The SS-18 implemented many original technical solutions. In particular, chemical pressurization of tanks, braking of separated stages by the expiration of pressurization gases, etc. An inertial control system was installed in the "Satan", operating with the help of an onboard digital computer complex. When using it, high accuracy of firing is ensured.

It also provides for launches even in the environment of the use of nuclear weapons by the enemy near the position of the missiles. "Satan" has a dark heat-shielding coating. It is easier for them to overcome the radiation dust clouds formed as a result of the use of nuclear weapons. Special sensors that measure gamma and neutron radiation when overcoming a nuclear “mushroom”, register it and turn off the control system, moreover, with functioning engines. At the exit from the danger zone, the control system turns on automatically and the flight path is corrected. Actually, these ICBMs had a particularly powerful combat equipment and a complex to overcome missile defense.

Be that as it may, the Satan ballistic missile still remains an unsurpassed and rather formidable Russian weapon to this day.

NATO gave the name "SS-18 "Satan" ("Satan") to a family of Russian missile systems with a heavy ground-based intercontinental ballistic missile, developed and put into service in the 1970s - 1980s. According to the official Russian classification, this is R- 36M, R-36M UTTH, R-36M2, RS-20. And the Americans called this missile "Satan" for the reason that it is difficult to shoot it down, and in the vast territories of the United States and Western Europe those Russian missiles will make hell.
SS-18 "Satan" was created under the leadership of chief designer V.F. Utkin. In terms of its characteristics, this missile surpasses the most powerful American missile, the Minuteman-3. "Satan" is the most powerful intercontinental ballistic missile on Earth. It is intended primarily , in order to destroy the most fortified command posts, ballistic missile silos and air bases.The nuclear explosive of one missile can destroy Big city, very most USA. Hit accuracy is about 200-250 meters. "The missile is located in the most durable mines in the world"; initial reports 2500-4500 psi, some mines 6000-7000 psi. This means that if there is no direct hit by American nuclear explosives on the mine, then the rocket will withstand a powerful blow, the hatch will open and "Satan" will fly out of the ground and rush towards the United States, where in half an hour it will give the Americans hell. And dozens of such missiles will rush to the United States. And each missile has ten individually targetable warheads. The power of the warheads is equal to 1,200 bombs dropped by the Americans on Hiroshima. With one blow, the Satan missile can destroy US and Western European facilities on an area of ​​​​up to 500 square meters. kilometers. And dozens of such missiles will fly in the direction of the United States. This is a complete kaput for Americans. "Satan" easily breaks through American system missile defense. She was invulnerable in the 80s and continues to be creepy for Americans today. The Americans will not be able to create reliable protection against the Russian "Satan" until 2015-2020. But even more frightening to the Americans is the fact that the Russians have begun developing even more satanic missiles.

“The SS-18 missile carries 16 platforms, one of which is loaded with decoys. Entering a high orbit, all the heads of the "Satan" go "in a cloud" of decoys and are practically not identified by radars.

But, even if the Americans see the "Satan" on the final segment of the trajectory, the heads of the "Satan" are practically not vulnerable to anti-missile weapons, because to destroy the "Satan" you only need a direct hit on the head of a very powerful anti-missile (and the Americans do not have anti-missiles with such characteristics ). “So such a defeat is very difficult and almost impossible with the level of American technology in the coming decades. As for the famous laser weapons for hitting the heads, in the SS-18 they are covered with massive armor with the addition of uranium-238, an exceptionally heavy and dense metal. Such armor cannot be "burned through" by a laser. In any case, those lasers that can be built in the next 30 years. Impulses cannot shoot down the SS-18 flight control system and its heads electromagnetic radiation, for all control systems of "Satan" are duplicated in addition to electronic, pneumatic machines "

Rocket Satan

SATANA - the most powerful nuclear intercontinental ballistic missile

By the middle of 1988, 308 intercontinental missiles "Satan" were ready to take off from the underground mines of the USSR in the direction of the USA and Western Europe. “Of the 308 launch silos that existed in the USSR at that time, Russia accounted for 157. The rest were in Ukraine and Belarus.” Each rocket has 10 warheads. The power of the warheads is equal to 1,200 bombs dropped by the Americans on Hiroshima. With one blow, the Satan missile can destroy US and Western European facilities on an area of ​​​​up to 500 square meters. kilometers. And such missiles will fly in the direction of the United States, if necessary, three hundred. This is a complete kaput for Americans and Western Europeans.

The development of the R-36M strategic missile system with a heavy intercontinental ballistic missile of the third generation 15A14 and a silo launcher with increased security 15P714 was carried out by Yuzhnoye Design Bureau. All the best developments obtained during the creation of the previous complex, R-36, were used in the new rocket.

The technical solutions used in the creation of the rocket made it possible to create the most powerful combat missile system in the world. He significantly surpassed his predecessor - R-36:

In terms of shooting accuracy - 3 times.
in terms of combat readiness - 4 times.
in terms of the energy capabilities of the rocket - 1.4 times.
according to the originally established warranty period of operation - 1.4 times.
in terms of launcher security - 15-30 times.
in terms of the degree of use of the volume of the launcher - 2.4 times.

The two-stage rocket R-36M was made according to the "tandem" scheme with a sequential arrangement of stages. To optimize the use of volume, dry compartments were excluded from the composition of the rocket, with the exception of the second stage interstage adapter. The applied design solutions made it possible to increase the fuel supply by 11% while maintaining the diameter and reducing the total length of the first two stages of the rocket by 400 mm compared to the 8K67 rocket.

At the first stage, the RD-264 propulsion system was used, consisting of four 15D117 single-chamber engines operating in a closed circuit, developed by KBEM ( chief designer- V.P. Glushko). The engines are pivotally fixed and their deviation on the commands of the control system provides control of the rocket's flight.

At the second stage, a propulsion system was used, consisting of a main single-chamber engine 15D7E (RD-0229) operating in a closed circuit and a four-chamber steering engine 15D83 (RD-0230) operating in an open circuit.

LRE rockets worked on high-boiling two-component self-igniting fuel. Unsymmetrical dimethylhydrazine (UDMH) was used as a fuel, and dinitrogen tetroxide (AT) was used as an oxidizing agent.

The separation of the first and second stages is gas-dynamic. It was provided by the operation of explosive bolts and the expiration of pressurization gases from fuel tanks through special windows.

Thanks to the improved pneumohydraulic system of the rocket with full ampulization of fuel systems after refueling and the exclusion of leakage of compressed gases from the rocket, it was possible to increase the time spent in full combat readiness up to 10-15 years with the potential for operation up to 25 years.

Schematic diagrams of the rocket and the control system were developed based on the condition of the possibility of using three variants of the warhead:

Light monoblock with a charge of 8 Mt and a flight range of 16,000 km;
Heavy monoblock with a charge of 25 Mt and a flight range of 11,200 km;
Multiple warhead (MIRV) of 8 warheads with a capacity of 1 Mt each;

All missile warheads were equipped with an improved set of means to overcome missile defense. For the first time, quasi-heavy decoys were created for the 15A14 missile defense penetration system. Thanks to the use of a special solid-propellant booster engine, the progressively increasing thrust of which compensates for the aerodynamic deceleration force of a decoy, it was possible to imitate the characteristics of warheads in almost all selective features in the extra-atmospheric trajectory and a significant part of the atmospheric one.

One of the technical innovations that largely determined high level characteristics of the new missile system was the use of a mortar launch rocket from a transport and launch container (TPK). For the first time in world practice, a mortar scheme for a heavy liquid ICBM was developed and implemented. At the start, the pressure created by the powder pressure accumulators pushed the rocket out of the TPK, and only after leaving the mine did the rocket engine start.

The missile, placed at the factory in a transport and launch container, was transported and installed in a mine launcher (silo) in an unfilled state. Refueling of the rocket with fuel components and docking of the warhead were carried out after the installation of the TPK with the rocket in the silo. Checks of on-board systems, preparation for launch and launch of the rocket were carried out automatically after the control system received the appropriate commands from a remote command post. To exclude unauthorized start, the control system accepted only commands with a certain code key for execution. The use of such an algorithm became possible due to the introduction of a new centralized control system at all command posts of the Strategic Missile Forces.

The missile control system is autonomous, inertial, three-channel with multi-tiered majority control. Each channel is self-tested. If the commands of all three channels did not match, the successfully tested channel took control. The onboard cable network (BCS) was considered absolutely reliable and was not rejected in the tests.

The acceleration of the gyroplatform (15L555) was carried out by forced acceleration machines (AFR) of digital ground equipment (CNA), and at the first stages of work - by software devices for accelerating the gyroplatform (PURG). Onboard digital Calculating machine(BTsVM) (15L579) 16-bit, ROM - memory cube. Programming was done in machine codes.

The developer of the control system (including the on-board computer) is the Design Bureau of Electrical Instrumentation (KBE, now JSC "Khartron", the city of Kharkov), the on-board computer was produced by the Kyiv Radio Plant, the control system was mass-produced at the Shevchenko and Kommunar plants (Kharkov).

The development of the third-generation strategic missile system R-36M UTTKh (GRAU index - 15P018, START code - RS-20B, according to the classification of the US Defense Ministry and NATO - SS-18 Mod.4) with a 15A18 missile equipped with a 10-unit multiple reentry vehicle has begun August 16, 1976.

The missile system was created as a result of the implementation of a program to improve and increase the combat effectiveness of the previously developed 15P014 (R-36M) complex. The complex ensures the defeat of up to 10 targets with one missile, including high-strength small-sized or extra-large area targets located on terrain up to 300,000 km², in conditions of effective counteraction by enemy missile defense systems. Improving the efficiency of the new complex was achieved due to:

Increasing the accuracy of shooting by 2-3 times;
increasing the number of warheads (BB) and the power of their charges;
increase in the area of ​​​​breeding BB;
the use of a highly protected silo launcher and command post;
increase the probability of bringing the launch commands to the silo.

The layout of the 15A18 rocket is similar to that of the 15A14. This is a two-stage rocket with a tandem arrangement of steps. As part of the new rocket, the first and second stages of the 15A14 rocket were used without modifications. The engine of the first stage is a four-chamber LRE RD-264 of a closed circuit. At the second stage, a single-chamber sustainer liquid-propellant rocket engine RD-0229 of a closed circuit and a four-chamber steering rocket engine RD-0257 of an open circuit are used. The separation of stages and the separation of the combat stage are gas-dynamic.

The main difference of the new rocket was the newly developed breeding stage and MIRV with ten new high-speed blocks, with increased power charges. The breeding stage engine is a four-chamber, dual-mode (thrust 2000 kgf and 800 kgf) with multiple (up to 25 times) switching between modes. This allows you to create the most optimal conditions for breeding all warheads. Another one design feature this engine - two fixed positions of the combustion chambers. In flight, they are located inside the breeding stage, but after separation of the stage from the rocket special arrangements the combustion chambers are taken out of the outer contour of the compartment and deployed to implement a "pulling" scheme for breeding warheads. The MIRV itself is made according to a two-tier scheme with a single aerodynamic fairing. Also, the memory capacity of the onboard computer was increased and the control system was upgraded to use improved algorithms. At the same time, the firing accuracy was improved by 2.5 times, and the launch readiness time was reduced to 62 seconds.

The R-36M UTTKh missile in a transport and launch container (TLC) is installed in a silo launcher and is on combat duty in a fueled state in full combat readiness. To load the TPK into the mine structure, SKB MAZ developed special transport and installation equipment in the form of a semi-trailer with a tractor based on the MAZ-537. The mortar method of launching a rocket is used.

Flight design tests of the R-36M UTTH rocket began on October 31, 1977 at the Baikonur test site. According to the flight test program, 19 launches were carried out, 2 of them were unsuccessful. The reasons for these failures were clarified and eliminated, the effectiveness of the measures taken was confirmed by subsequent launches. A total of 62 launches were carried out, of which 56 were successful.

On September 18, 1979, three missile regiments began combat duty at the new missile system. As of 1987, 308 R-36M UTTKh ICBMs were deployed as part of five missile divisions. As of May 2006, the Strategic Missile Forces included 74 silo launchers with R-36M UTTKh and R-36M2 ICBMs, each equipped with 10 warheads.

The high reliability of the complex was confirmed by 159 launches as of September 2000, of which only four were unsuccessful. These failures during the launch of serial products are due to manufacturing defects.

After the collapse of the USSR and economic crisis At the beginning of the 1990s, the question arose of extending the service life of the R-36M UTTKh until they were replaced by new Russian-designed complexes. For this, on April 17, 1997, the R-36M UTTKh missile, manufactured 19.5 years ago, was successfully launched. NPO Yuzhnoye and the 4th Central Research Institute of the Ministry of Defense carried out work to increase the warranty period for missiles from 10 years consecutively to 15, 18 and 20 years. On April 15, 1998, a training launch of the R-36M UTTKh rocket was carried out from the Baikonur Cosmodrome, during which ten training warheads hit all learning goals at the Kura training ground in Kamchatka.

A joint Russian-Ukrainian venture was also created for the development and further commercial use of the launch vehicle. light class"Dnepr" on the basis of missiles R-36M UTTH and R-36M2

On August 9, 1983, by a decree of the Council of Ministers of the USSR, Yuzhnoye Design Bureau was tasked with finalizing the R-36M UTTKh missile so that it could overcome the promising American missile defense (ABM) system. In addition, it was necessary to increase the protection of the rocket and the entire complex from the action damaging factors nuclear explosion.
View of the instrument compartment (breeding stage) of the 15A18M rocket from the head end. The elements of the breeding engine are visible (aluminum colors - fuel and oxidizer tanks, green - ball cylinders of the displacement supply system), control system instruments (brown and aqua).
The upper bottom of the first stage 15A18M. On the right is the undocked second stage, one of the steering engine nozzles is visible.

The fourth-generation missile system R-36M2 "Voevoda" (GRAU index - 15P018M, START code - RS-20V, according to the classification of the US Defense Ministry and NATO - SS-18 Mod.5 / Mod.6) with a multi-purpose heavy-class intercontinental missile 15A18M is designed for destruction of all types of targets protected modern means ABM, in any conditions of combat use, including with multiple nuclear impact on the positional area. Its use makes it possible to implement the strategy of a guaranteed retaliatory strike.

As a result of applying the latest technical solutions, the energy capabilities of the 15A18M rocket have been increased by 12% compared to the 15A18 rocket. At the same time, all the conditions for restrictions on dimensions and starting weight imposed by the SALT-2 agreement are met. Missiles of this type are the most powerful of all intercontinental missiles. The technological level of the complex has no analogues in the world. Used in the missile system active protection a silo launcher from nuclear warheads and high-precision non-nuclear weapons, as well as for the first time in the country, a low-altitude non-nuclear interception of high-speed ballistic targets was carried out.

Compared with the prototype, the new complex managed to improve many characteristics:

Increasing the accuracy by 1.3 times;
increase in 3 times the duration of autonomy;
reduction in 2 times the time of combat readiness.
increasing the area of ​​the warhead disengagement zone by 2.3 times;
the use of high-power charges (10 individually targetable multiple warheads with a capacity of 550 to 750 kt each; total throw weight - 8800 kg);
the possibility of launching from the mode of constant combat readiness according to one of the planned target designations, as well as operational retargeting and launching according to any unscheduled target designation transferred from the top management;

To ensure high combat effectiveness in especially difficult conditions combat use in the development of the R-36M2 "Voevoda" complex, special attention was paid to the following areas:

Improving the security and survivability of silos and command posts;
sustainability combat control in all conditions of application of the complex;
increasing the autonomy of the complex;
increase in the warranty period of operation;
ensuring the resistance of the rocket in flight to the damaging factors of ground and high-altitude nuclear explosions;
expansion of operational capabilities for retargeting missiles.

One of the main advantages of the new complex is the ability to provide missile launches in the conditions of a retaliatory strike under the influence of ground and high-altitude nuclear explosions. This was achieved by increasing the survivability of the rocket in the silo launcher and a significant increase in the resistance of the rocket in flight to the damaging factors of a nuclear explosion. The rocket body has a multifunctional coating, protection of the control system equipment from gamma radiation has been introduced, the speed of the executive bodies of the control system stabilization machine has been increased by 2 times, the separation of the head fairing is carried out after passing through the zone of high-altitude blocking nuclear explosions, the engines of the first and second stages of the rocket are boosted by thrust.

As a result, the radius of the missile's impact zone with a blocking nuclear explosion, in comparison with the 15A18 missile, is reduced by 20 times, resistance to X-ray radiation is increased by 10 times, and to gamma-neutron radiation - by 100 times. The resistance of the rocket to the impact of dust formations and large particles of soil, which are present in the cloud during a ground-based nuclear explosion, is ensured.

For the rocket, silos with ultra-high protection against damaging factors of nuclear weapons were built by re-equipping the silos of the 15A14 and 15A18 missile systems. The implemented levels of missile resistance to damaging factors of a nuclear explosion ensure its successful launch after a non-damaging nuclear explosion directly at the launcher and without reducing combat readiness when exposed to a neighboring launcher.

The rocket is made according to a two-stage scheme with a sequential arrangement of stages. The rocket uses similar launch schemes, stage separation, warhead separation, breeding of combat equipment elements, which have shown a high level of technical excellence and reliability as part of the 15A18 rocket.

The propulsion system of the first stage of the rocket includes four hinged single-chamber rocket engines with a turbopump fuel supply system and made in a closed circuit.

The propulsion system of the second stage includes two engines: a sustainer single-chamber RD-0255 with a turbopump supply of fuel components, made according to a closed circuit and a steering RD-0257, a four-chamber, open circuit, previously used on the 15A18 rocket. The engines of all stages operate on liquid high-boiling fuel components UDMH + AT, the stages are fully ampulized.

The control system was developed on the basis of two high-performance central control centers (onboard and ground) of a new generation and a high-precision complex of command devices continuously operating during combat duty.

A new head fairing has been developed for the rocket, which provides reliable protection of the warhead from the damaging factors of a nuclear explosion. The tactical and technical requirements provided for equipping the rocket with four types of warheads:

Two monoblock MS - with "heavy" and "light" BB;
MIRV with ten unguided BBs with a power of 0.8 Mt;
Mixed MIRV consisting of six unmanaged and four controlled warheads with a homing system based on terrain maps.

As part of the combat equipment, highly effective systems for overcoming missile defense (“heavy” and “light” decoys, dipole reflectors) were created, which are placed in special cassettes, thermally insulating covers of the BB are used.

Flight design tests of the R-36M2 complex began at Baikonur in 1986. The first launch on March 21 ended in an accident: due to an error in the control system, the first stage propulsion system did not start. The rocket, leaving the TPK, immediately fell into the shaft of the mine, its explosion completely destroyed the launcher. There were no human casualties.

The first missile regiment with R-36M2 ICBMs went on combat duty on July 30, 1988. On August 11, 1988, the missile system was put into service. Flight design tests of the new fourth-generation intercontinental missile R-36M2 (15A18M - "Voevoda") with all types of combat equipment were completed in September 1989. As of May 2006, the Strategic Missile Forces included 74 mine launchers with R-36M UTTKh and R-36M2 ICBMs equipped with 10 warheads each.

December 21, 2006 at 11:20 Moscow time, a combat training launch of the RS-20V was carried out. According to the head of the information and public relations service of the Strategic Missile Forces, Colonel Alexander Vovk, the combat training units of the rocket launched from the Orenburg region (Urals) hit mock targets with the specified accuracy at the Kura training ground on the Kamchatka Peninsula in pacific ocean. The first stage fell in the zone of Vagaisky, Vikulovsky and Sorokinsky districts of the Tyumen region. She separated at an altitude of 90 kilometers, the remnants of the fuel burned out during the fall to the ground. The launch took place as part of the Zaryadye development work. The launches gave an affirmative answer to the question of the possibility of operating the R-36M2 complex for 20 years.

On December 24, 2009 at 9:30 Moscow time, an intercontinental ballistic missile RS-20V (“Voevoda”), Colonel Vadim Koval, spokesman for the press service and information department of the Ministry of Defense for the Strategic Missile Forces, said: “On December 24, 2009, at 9.30 Moscow time, the Strategic Missile Forces launched a missile from the positional area of ​​​​the formation stationed in the Orenburg region, " Koval said. According to him, the launch was carried out as part of development work in order to confirm flight performance RS-20V missiles and extending the life of the Voevoda missile system to 23 years.