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Contents

   



(Top)
 


1 History  





2 Operations  



2.1  Command and Control  







3 Flight test history  



3.1  Test Launches  







4 General Characteristics  





5 Operators  





6 Photo gallery  





7 See also  





8 References  





9 External links  














RT-2






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From Wikipedia, the free encyclopedia
 


RT-2
SS-13 Savage
TypeIntercontinental ballistic missile
Place of originSoviet Union
Service history
In service1968-1976
Used bySoviet Strategic Rocket Forces
Specifications
Mass45,100 kg (99,400 lb)
Length21.5 m (71 ft)
Diameter1.7 m (5 ft 7 in)

EngineThree-stage solid propellant

Operational
range

10,000 km

Guidance
system

autonomous inertial guidance
AccuracyMaximum 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[1] until 1976.[2] It was assigned the NATO reporting name SS-13 Savage and carried the GRAU index 8K98. Designed by OKB-1,[1] about 60 were built by 1972.

History

[edit]

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 missile. 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[citation needed]

Operations

[edit]

The RT-2 was capable of delivering a 540 kg (1,200 lb) class payload to a maximum operational range of approximately 10,000 km (5,500 nautical miles)[3]

Command and Control

[edit]

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.

Flight test history

[edit]

Test Launches

[edit]
RT-2 Test Launches
Date System Location Range (NM) Note
26 Feb 1966 RT-2 Mod Kapustin Yar

General Characteristics

[edit]
An RT-2

Operators

[edit]
 Soviet Union
The Strategic Rocket Forces were the only operator of the RT-2.
[edit]

See also

[edit]

References

[edit]
  1. ^ a b "Rocket RT-2P". RKK Energia. Retrieved 17 January 2012.
  • ^ Zak, Anatoly. "RT-2". RussianSpaceWeb. Retrieved 17 January 2012.
  • ^ Defense Intelligence Agency: "SS-13 Ballistic Missile System", 8 November 1973, DIA Task No. T74-10-03
  • [edit]


    Retrieved from "https://en.wikipedia.org/w/index.php?title=RT-2&oldid=1139369364"

    Categories: 
    Cold War intercontinental ballistic missiles of the Soviet Union
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    This page was last edited on 14 February 2023, at 19:49 (UTC).

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