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R-36M2 Voevoda

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Article Genealogy
Parent: RS-28 Sarmat Hop 4
Expansion Funnel Raw 36 → Dedup 8 → NER 3 → Enqueued 2
1. Extracted36
2. After dedup8 (None)
3. After NER3 (None)
Rejected: 5 (not NE: 5)
4. Enqueued2 (None)
Similarity rejected: 1
R-36M2 Voevoda
NameR-36M2 Voevoda
TypeIntercontinental ballistic missile
OriginSoviet Union
Used bySoviet Union, Russia
DesignerYuzhnoye Design Office
ManufacturerYuzhmash
Production date1988–1992
Service1988–present
EngineTwo-stage liquid-propellant
Weight211,400 kg
Length34.3 m
Diameter3.0 m
Vehicle range11,000–16,000 km
GuidanceInertial, autonomous
Launch platformSilo-based

R-36M2 Voevoda. It is a Russian intercontinental ballistic missile (ICBM), representing the final and most formidable evolution of the R-36 family developed by the Soviet Union. Designed by the Yuzhnoye Design Office and manufactured at Yuzhmash in Ukraine, it entered service in 1988 as a direct response to advanced United States missile defense concepts like the Strategic Defense Initiative. Renowned for its massive throw weight and formidable MIRV capability, it remains a cornerstone of Russia's strategic nuclear deterrent.

Development and design

The development of this system was initiated in the early 1980s under the direction of chief designer Vladimir Utkin at the Yuzhnoye Design Office. The primary design goal was to overcome projected United States ABM systems, particularly those envisioned under President Ronald Reagan's Strategic Defense Initiative. Engineers focused on significantly reducing the missile's vulnerable boost phase and enhancing its ability to penetrate enemy defenses. Key innovations included a fast-burn, storable liquid-propellant first stage, a redesigned post-boost vehicle, and advanced penetration aids including decoys. The missile was engineered for a "launch-on-warning" posture, with the ability to be fired from its hardened silos within minutes of a confirmed attack, ensuring retaliation even after a first strike.

Operational history

The system was officially deployed with the Strategic Rocket Forces in 1988, with the final missiles entering service in 1992. Following the Dissolution of the Soviet Union, all deployed missiles fell under the command of the newly formed Russian Federation. Its operational life was extended multiple times, far beyond its original service window, due to ongoing modernization programs. Under the terms of the START I and New START treaties, the number of deployed launchers was progressively reduced. The missile has been a consistent subject of arms control discussions and tensions, particularly concerning its testing and the involvement of the Yuzhmash factory in post-Soviet Ukraine. It remains on active, combat-alert duty in Russia's nuclear arsenal to this day.

Technical specifications

The missile is a two-stage, liquid-propelled ICBM with a launch weight of approximately 211,400 kg and a length of 34.3 meters. It possesses an operational range between 11,000 and 16,000 kilometers, capable of delivering its payload anywhere on the globe. Its most notable feature is a massive throw weight of 8,800 kg, which allows it to carry up to ten MIRV warheads, each with a yield estimated between 550 and 750 kt. Alternatively, it can be fitted with a single high-yield warhead of up to 20 Mt. Guidance is provided by a sophisticated, autonomous inertial navigation system housed in the post-boost vehicle, ensuring high accuracy with a reported CEP of 220–500 meters. The missile is launched from a heavily fortified and hardened Silo, designed to withstand significant overpressure from nearby nuclear detonations.

Variants and upgrades

The primary variant is the 15A18M missile, which is the standard MIRV-equipped system. A dedicated version, designated 15A18M2, was developed to carry the Avangard hypersonic glide vehicle, a program initiated in the late 1980s under the project name Project 4202. This upgrade involved modifying the existing missile's post-boost vehicle to release the boost-glide payload. While the basic airframe has remained consistent, numerous service-life extension programs have been conducted by organizations like the Makeyev Rocket Design Bureau, updating its electronics, solid-fuel components, and support systems. These upgrades have ensured its continued reliability and operational relevance decades after its initial deployment, effectively creating a new, modernized version without altering its core designation.

Strategic role and legacy

Codenamed SS-18 Satan by NATO, it has been perceived as the most powerful ICBM ever deployed, forming the heavy backbone of Russia's land-based strategic forces. Its primary strategic role is to guarantee a devastating retaliatory second strike, capable of overwhelming any existing or prospective missile defense shield, such as the Ground-Based Midcourse Defense system. The missile's sheer size, payload, and hard-target kill capability made it a central element of the doctrine of Mutual assured destruction during the Cold War. Its enduring service life and adaptation to carry next-generation payloads like the Avangard ensure its legacy continues to shape global strategic stability and arms control dynamics between Russia and the United States.

Category:Intercontinental ballistic missiles of the Soviet Union Category:Intercontinental ballistic missiles of Russia Category:Cold War missiles of the Soviet Union