R-2 (missile)
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The R-2 (NATO reporting name SS-2 Sibling) was a Soviet short-range ballistic missile developed from and having twice the range as the R-1 missile (itself a copy of the German V-2). Developed from 1946-1951, the R-2 entered service in numbers in 1953 and was deployed in mobile units throughout the Soviet Union until 1962. A sounding rocket derivative, the R-2A, tested a prototype of the dog-carrying capsule flown on Sputnik 2 in 1957. The same year, the R-2 was licensed for production in the People's Republic of China, where it entered service as the Dongfeng 1.
History
In 1945 the Soviets captured several key A-4 (V-2) rocket production facilities, and also gained the services of some German scientists and engineers related to the project. Under the supervision of the Special technical Commission (OTK) established by the Soviet Union to oversee rocketry operations in Germany, A-4s were assembled and studied. This prompted the 13 May 1946 decree of the Soviet Council of Ministers for, in part, the development of a Soviet copy of the A-4, which would be the first domestically produced ballistic missile. A further decree on 16 May converted the M.I. Kalinin Plant No. 88, which had produced artillery and tanks during World War II into NII-88, tasked with managing the Soviet Union's long-range rocketry programs.<ref name=challenge>Template:Cite book</ref>Template:Rp In April 1947 Josef Stalin authorized the production of the R-1 missile, the designation for the Soviet copy of V-2.<ref name=astror1>Template:Cite web</ref> NII-88 chief designer Sergei Korolev oversaw the R-1's development.<ref name=challenge/>Template:Rp Testing of the R-1 proceeded from 1948 to 1950,<ref name=ranp>Template:Cite book</ref>Template:Rp and the R-1 missile system entered into service in the Soviet Army on 28 November 1950.<ref name="Zaloga20132">Template:Cite book</ref><ref name="Zaloga2013">Template:Cite book</ref>
By the latter half of 1946, Korolev and rocket engineer Valentin Glushko had, with extensive input from German engineers, outlined a successor to the R-1 with an extended frame and a new engine designed by Glushko.<ref name=challenge/>Template:Rp The R-2 would have a range of Template:Convert, twice that of the R-1, while maintaining a similar payload of around Template:Convert.<ref name=ranp/>Template:Rp
Korolev proposed commencement of the R-2 project in January 1947, but it was declined by the Soviet government, which favored development of the more technologically conservative R-1.<ref name=challenge/>Template:Rp Moreover, development of the R-2 was in direct competition with the G-1 missile being concurrently developed by Helmut Gröttrup, head of a German team of engineers. Though the G-1 was a compelling design, able to lift a payload three times heavier than that of the A-4, and with higher precision and a shorter launch preparation time, it was politically infeasible to leave the Soviet missile program in the hands of Germans. Thus, on April 14, 1948, the same decree that authorized the operational production of the R-1 also sanctioned development of the R-2. The G-1 was ultimately never completed.<ref name=challenge/>Template:Rp
Description
Like its predecessor, the R-1, the R-2 was a single-stage missile using ethanol as a fuel and liquid oxygen as an oxidizer.<ref name=ranp/>Template:Rp At a length of Template:Cvt and a mass of Template:Cvt, the R-2 was Template:Cvt longer and the dry weight of Template:Cvt was about Template:Cvt heavier than the R-1.<ref name="R-2Zak">Template:Cite web</ref> Maximum body diameter remained Template:Cvt, the same as the R-1,<ref name=challenge/>Template:Rp and in the interests of conservatism, the R-2 retained the R-1's graphite stabilizing fins, though they reduced lifting capacity and caused heating and stress issues.<ref name=challenge/>Template:Rp
The R-2 design included four major improvements over the R-1:
- The warhead separated from the rocket prior to atmospheric reentry, enhancing hull strength (one of the V-2/R-1's biggest weaknesses)<ref name=challenge/>Template:Rp and increasing range.<ref name=challenge/>Template:Rp
- The propellant tank became the main load-bearing structure for the rocket, in contrast to the R-1's load-bearing hull. This reduced the overall weight of the spaceframe.<ref name=challenge/>Template:Rp
- The R-2 had much improved command guidance, and access to the unit was made easier to reduce prelaunch preparation time.<ref name=challenge/>Template:Rp
- The RD-101 engine was 50% more powerful than the RD-100 used by the R-1.<ref name=astror1/><ref name=astror2/> This increased performance was made possible by raising combustion pressure and increasing the concentration of ethanol fuel.<ref name=challenge/>Template:Rp
Development
Test launches of an experimental version of the R-2, designated R-2E, began on 25 September 1949. Five of these slightly shorter (Template:Cvt) rockets were fired from Kapustin Yar, three of them successfully. The R-1A, a variant of the R-1 developed largely to test the separable warhead concept to be used in the R-2, was also test-flown in 1949. Launches of the full-scale R-2 began on 21 October 1950, the last being fired on 20 December. None of the 12 flights in this series fulfilled their primary objectives due to engine failures, warhead trajectory errors, and malfunctions with the guidance systems.<ref name=challenge/>Template:Rp
A second series of tests was carried out between 2-27 July, 1951. The R-2 had been made more reliable by then, and twelve of the thirteen flights successfully reached their targets.<ref name=challenge/>Template:Rp A subsequent series of 18 launches in 1951 had 14 successes.<ref name="astror2" /><ref name=ranp/>Template:Rp Per an order dated 27 November, 1951, the R-2 was formally adopted as operational armament for the Soviet Union,<ref name=challenge/>Template:Rp and production was authorized at factory 586 in Dnepropetrovsk three days later. Mass production began at this factory in June 1953.<ref name=astror2/> As with the R-1, reliability remained suboptimal. In a series of 14 operational R-2s test-launched in 1952, only 12 reached their target.<ref name=ranp/>Template:Rp
Military service
The R-2 was deployed in Supreme Command Reserve (RVGK) engineer brigades<ref name=ranp/>Template:Rp consisting of three divizions each equipped with two rockets and mobile launch equipment. A crew of 11 was required for the launch of each missile, preparations for which took six hours, including 15 minutes for guidance system programming. After preparation, a rocket could stand ready to fire for 24 hours before it required defueling and renewed preparations. The R-2 was launched operationally in temperatures ranging from Template:Cvt to Template:Cvt, withstanding wind speeds of up to Template:Cvt. <ref name=astror2>Template:Cite web</ref>
The first two R-2 military units, the 54th and 56th brigades, were formed for the 1952 test launches. Starting in 1953, divisions were deployed to Zhytomyr; Kolomyia; Template:Ill, Novgorod Oblast; Kamyshin, Volgograd Oblast; Šiauliai, Lithuanian SSR; Dzhambul, Kazakh SSR; and Ordzhonikidze, and in the Far East.<ref name=astror2/> The R-2 was retired from active service in 1962.<ref name=Podvig119/>
Like the R-1, the R-2's utility was limited by the smallness of its warhead. The Geran (Eng: Geranium) radiological warhead, which would disperse radioactive liquid as toxic rain around the impact point, was proposed for use with the R-2. However, this warhead was ultimately never developed.<ref name=ranp/>Template:Rp
The West obtained its first photographs of the R-2 (which they designated SS-2 "Sibling") in December 1959 when aerial surveillance returned images from rockets deployed at Kapustin Yar. These confirmed the dimensions of the rocket and revealed much information about the organization of the RVGK brigades.<ref name=program>Template:Cite web</ref>
R-2A sounding rocket
The R-2 had a maximum altitude of Template:Cvt, a two-fold improvement over that of the R-1. This made it a much more desirable vehicle for probing outer space. OKB-1 developed a draft plan for the R-2A sounding rocket in 1956. This new vehicle would loft a Template:Cvt capsule housing two dogs and also two Template:Cvt strap-on pods for scientific experiments.<ref name=challenge/>Template:Rp
A first series of five launches, each carrying a pair of dogs, was carried out from 16 May 1957 through 9 September. During these flights, the animals experienced several minutes of weightlessness. Just two months later, Sputnik 2 was launched into orbit containing a canine passenger inside a capsule derived from the one used on the R-2A.<ref name=challenge/>Template:Rp Sounding rocket flights continued through 1960 with biological and ionospheric packages.<ref name=astror2a>Template:Cite web</ref>
Originally, OKB-1 planned to use the R2A for suborbital human test flights. This was on the assumption that a human orbital flight would not be feasible until the mid '60s. With the completion of the R-7 Semyorka ICBM, however, it became clear that a crewed mission into orbit would happen much sooner, and the plan was abandoned.<ref name=challenge/>Template:Rp
Chinese version (Dongfeng 1)
On 6 December 1957 an agreement was signed to license production of the R-2 to China,<ref name=astror2/> which was produced as the Dongfeng 1.<ref name=astnow>Template:Cite web</ref> In August 1958, a group of OKB-1 senior engineers and several R-2 missiles were sent to China in aid of that country's fledgling ballistic missile program.<ref name=challenge/>Template:Rp This team was sent home 2 August 1960 amidst increased tension between the Soviet Union and China.<ref name=astnow/>
Operators
See also
References
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