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R-11 Zemlya
Soviet tactical ballistic missile
Soviet tactical ballistic missile
| Field | Value |
|---|---|
| name | R-11 Zemlya |
| image | 2P19 Transporter-Erector-Launcher with 8K14 rocket of 9K72 missile complex «Elbrus», Artillery museum, Saint-Petersburg pic3.JPG |
| origin | Soviet Union |
| type | Short-range ballistic missile |
| is_vehicle | yes |
| is_missile | yes |
| service | 1956-1978 |
| production_date | 1956-1962 |
| weight | 5.4 tonnes |
| length | 10 604 mm |
| diameter | 880 mm |
| max_range | 170 km |
| filling | HE, nuclear |
The R-11 Zemlya (), GRAU index 8A61 was a Soviet tactical ballistic missile. It is also known by its NATO reporting name SS-1b Scud-A. It was the first of several similar Soviet missiles to be given the reporting name Scud. Variant R-11M was accepted into service, with GRAU index 9K51 (9К51).
Origin
The R-11 originated from a 1951 requirement for a ballistic missile with similar performance to the German V-2 rocket, but half its size. With the Wasserfall, an anti-aircraft version of the V-2, as a model the R-11 was developed by engineer Victor Makeev, who was then working in OKB-1, headed by Sergey Korolyov. The two men agreed on the use of RG-1 as the fuel, but disagreed over which oxidizer to use, with Korolev favouring the use of liquid oxygen, while Makeev advocated the use of a storable but toxic oxidizer. Makeev's version, that first flew on 18 April 1953, was fitted with an Isayev engine using RG-1 and nitric acid. On 13 December 1953, a production order was passed with SKB-385 in Zlatoust, a factory dedicated to producing long-range rockets. In June 1955, Makeev was appointed chief designer of the SKB-385 to oversee the programme and, in July, the R-11 was formally accepted into military service. The definitive R-11M, designed to carry a nuclear warhead, was accepted officially into service on 1 April 1958. The launch system received the GRAU index 9K51, the rocket itself 8K11, and the launcher 8U218.
Systems specification

Like the V-2, the R-11 relied on inertial guidance, and its flight was controlled by four graphite vanes in the engine exhaust, that were active only while the motor was burning. The R-11M had a maximum range of 270 km, but when carrying a nuclear warhead, this was reduced to 170 km, hence an alternative designation R-170. At maximum range, it was found to have an average range error 1.19 km and an azimuth error of 660 m. It was used as a mobile nuclear strike vector, giving the Soviet Army the ability to hit European targets from forward areas. To give the system sufficient mobility on the battlefield, the R-11 was mounted on the chassis of an IS-2 tank, that became its first transporter erector launcher 8U218. Main payload was a nuclear warhead with an estimated yield of 10, 20 or 40 kilotons. There was also HE-Frag warhead 9N33 with 535 kg of explosive.
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Users
- Soviet Union
- Polish People's Republic
- Socialist Republic of Romania
References
References
- [http://www.johnstonsarchive.net/nuclear/sovietmissiledes.html Johnston's Archive – Soviet/Russian Missile Designations]
- Wade, Mark. "R-11". [[Encyclopedia Astronautica]].
- Rochowicz, Robert (2018) (in Polish). ''Rakiety operacyjne i taktyczne w Siłach Zbrojnych PRL''. „Poligon” No. 1/2018(62), pp. 56–63, {{ISSN. 1895-3344
- Zaloga, p. 4
- "Rocket R-11".
- Zaloga, p. 8
- (July 13, 2000). "R-11FM / SS-1b Scud". [[Federation of American Scientists]].
- "WYRZUTNIA RAKIET OPERACYJNO-TAKTYCZNYCH R 170".
- (2010). "Artileria Română în date și imagini". Editura Centrului Tehnic-Editorial al Armatei.
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