Missile RT-23 Molodets (SS-24 Scalpel)
Ex-USSR ICBM, entered service in 1987, deployed on railroad cars for increased survivability. Key figures: range 10,000 km, top speed 24,000 km/h, guidance Inertial, autonomous, in service since 1987. In service with 2 countries β Russia, Ukraine.
| Warhead | 10 nuclear MIRV |
| Nuclear yield | 550 kt |
| Diameter | 2,400 mm (94.5 in) |
| Length | 22,400 mm (881.9 in) |
| Weight | 104,500 kg (230,383 lb) |
| Range | 10,000 km (6,214 mi) |
| Max. speed | 24,000 km/h (Mach 24.0) |
See what a 550 kt strike from the RT-23 Molodets would do to a real city: set ground zero anywhere on Earth and map the fireball, blast, thermal and radiation rings.
Description
The RT-23 Molodets originated from a 1969 Soviet program to develop a solid-propellant ICBM capable of multiple basing modes. The system was intended to replace the liquid-fueled UR-100N. Development included silo-based and rail-based variants, though a proposed road-mobile version was rejected. Flight testing occurred during the 1980s, and the system entered service in 1987.
The RT-23 is a cold-launched, three-stage, solid-fueled intercontinental ballistic missile utilizing an autonomous inertial guidance system. The missile is armed with ten Multiple Independently Targetable Reentry Vehicles (MIRVs), each with a 550 kt yield.
The rail-based variant, designated BZhRK, operates from a train consisting of three locomotives and seventeen cars camouflaged as civilian refrigerated vans or passenger rail. Each train includes three autonomous launching modules, command posts, and support systems, allowing for autonomous operation for up to 28 days. To accommodate the missile within railcar dimensions, the rail-based version utilizes an inflatable nose cone, while the silo-based variant uses a folding nose cone designed for protection during nuclear strikes. Launch from the railcar involves a powder pressure accumulator that ejects the missile to a height of 20β30 meters. The missile then inclines away from the train before first-stage ignition to prevent exhaust damage to the launcher. To prevent railroad track damage from the weight of the launching car, a three-car coupling system distributes weight between neighboring cars. The rail system was tested for resilience against electromagnetic pulses, lightning, and the effects of nearby nuclear detonations.
The RT-23 was operated by the Strategic Rocket Forces of the Soviet Union. Following the dissolution of the USSR, missiles were located in Russia and Ukraine. Ukrainian forces inherited silo-based units, which were deactivated by the mid-1990s. These missiles were dismantled and their silos destroyed, with warheads transferred to Russia for dismantlement. In Russia, the system was deployed in silo and rail-based configurations across several rocket divisions. Silo-based missiles were deactivated by 2001, and their silos were modified for subsequent missile complexes. The rail-based complexes were gradually withdrawn from service after 2000. All RT-23 units were decommissioned by 2005 in compliance with the START II treaty, and the final missile was eliminated in 2008.
Frequently Asked Questions
What type of missile is the RT-23 Molodets?
What is the range of the RT-23 Molodets?
How fast is the RT-23 Molodets?
What warhead does the RT-23 Molodets carry?
How is the RT-23 Molodets guided?
Which countries use the RT-23 Molodets?
- FEB 72026 Updated Warhead yield updated
- JAN 242026 Updated Max speed added
- JAN 192026 Updated Description, number built and 3 more fields added
- JAN 182026 Updated Sources and cross-references refreshed