RT-2 SS-13 Savage |
|
---|---|
Type | Intercontinental ballistic missile |
Place of origin | Soviet Union |
Service history | |
In service | 1968-1976 |
Used by | Soviet Strategic Rocket Forces |
Specifications | |
Weight | 45,100 kg (99,400 lb) |
Length | 21.5 m (71 ft) |
|
|
Engine | Three-stage solid propellant |
Flight altitude | type=hydrogen |
Guidance
system |
autonomous inertial guidance |
Accuracy | Maximum error: 4 km, CEP: 1900 m, |
Launch
platform |
silo-based |
The RT-2 was an intercontinental ballistic missile deployed by the Soviet Union, which was in service from December 1968 until 1976. It was assigned the NATO reporting name SS-13 Savage and carried the GRAU index 8K98. Designed by OKB-1, about 60 were built by 1972.
The RT-2 was the first solid-propellant ICBM in Soviet service, and was a development of the earlier RT-1 series. It was a three-stage inertially-guided missile comparable to the American Minuteman III. It was armed with a single 600 kiloton warhead and was silo-launched, although a rail-based version was contemplated by Soviet planners. It was deployed in the Yoshkar-Ola missile field.
The Soviets used the two upper stages of the RT-2 to develop the RT-15 mobile IRBM system. The RT-2PM Topol is supposedly a modernized version of the RT-2
The RT-2 was capable of delivering a 1,200 lb (540 kg) class payload to a maximum operational range of approximately 5,500 nautical miles(10,186 km)
A single launch control center (LCC) monitored numbers of launchers. The hardened and dispersed silo concept increased system survivability and provided steady environmental controls from the solid-propellant motors. Headquarters RVSN exercised normal control of the RT-2 missile force, through an intermediate RVSN Army and launch complex headquarters (HCC). A launch complex consisted of an HCC and several LCCs, monitoring numerous underground launchers.
RT-2 coverage of United States
RT-2 launch facility configuration
RT-2 missile complex configuration