R-7 Semyorka

For the rocket used to launch Sputnik 1, see Sputnik (rocket). For other R-7 derived carrier rockets, see R-7 (rocket family).
R-7A

A 2-view drawing of the R-7 Semyorka (NATO code-name SS-6 Sapwood)
Type Ballistic Missile
Place of origin Soviet Union
Service history
In service 9 February 1959 - 1968
Used by  Soviet Union: Strategic Missile Troops
Wars Cold War
Production history
Designer Sergei Korolev
Designed From 1953
Manufacturer OKB-1
Specifications
Weight 280 metric tons (280 long tons; 310 short tons)
Length 34 m (112 ft)
Diameter 3.02 m (9.9 ft)
Engine

1st stage: 4x jettisonable four-chamber RD-107 booster engines each with 2x vernier rocket engines plus 1x four-chamber RD-108 core engine with 4x vernier rocket engines.
2nd stage: 1x four-chamber RD-108 core engine with 4x vernier rocket engines.
RD-107 4x 907.4 kN (203,992 lbf)
RD-108 1x 907.4 kN (203,992 lbf)

Vernier 12x 38.259 kN (8,601 lbf)
Propellant Kerosene T-1 fuel + liquid oxygen (LO2) Oxidiser.
Guidance
system
 Inertial guidance with radio control of vernier thrusters for launch.
Steering
system
 12x vernier thrusters arranged around the booster clusters and the core engines
Accuracy 2.5-5.0 kilometers (max. deviation 10 kilometers)

The R-7 (Russian: Р-7 «Семёрка») was a Soviet missile developed during the Cold War, and the world's first intercontinental ballistic missile.[1] The R-7 made 28 launches between 1957 and 1961, but was never deployed operationally. A derivative, the R-7A, was deployed from 1959 to 1968. To the West it was known by the NATO reporting name SS-6 Sapwood and within the Soviet Union by the GRAU index 8K71. In modified form, it launched Sputnik 1, the first artificial satellite, into orbit, and became the basis for the R7 family which includes Sputnik, Luna, Molniya, Vostok, and Voskhod space launchers, as well as later Soyuz variants.

The widely used nickname for the R-7 launcher, "semyorka", means "the 7" in Russian.

Description

The R-7 was 34 m (112 ft) long, 3.02 m (9.9 ft) in diameter and weighed 280 metric tons (280 long tons; 310 short tons); it had two stages, powered by rocket engines using liquid oxygen (LOX) and kerosene and capable of delivering its payload up to 8,800 km (5,500 mi), with an accuracy (CEP) of around 5 km (3.1 mi). A single thermonuclear warhead was carried with a nominal yield of 3 megatons of TNT. The initial launch was boosted by four strap-on liquid rocket boosters making up the first stage, with a central 'sustainer' motor powering through both the first and the second stage. Each strap-on booster included two vernier thrusters and the core stage included four.[2] The guidance system was inertial with radio control of the vernier thrusters.

Development

Design work began in 1953 at OKB-1 in Kaliningrad in Moscow oblast (presently Korolev, Moscow Oblast) and other divisions with the requirement for a two-stage missile of 170 metric tons (170 long tons; 190 short tons) with a range of 8,000 km (5,000 mi) carrying a 3,000 kg (6,600 lb) warhead. Following first ground tests in late 1953 the initial design was heavily reworked and the final design was not approved until May 1954 and Korolev reportedly reviewed more than 100 design proposals. In 1954 draft project was completed. For the first time in the history of the development of the conceptual design firm Sergei Pavlovich Korolev was created, received the room volume № 14. This volume was developed under the leadership of the Arcady Ilyich Ostashev and devoted to the organization of test missiles.

Contrary to statements that the R-7 was based largely on experience and assistance of German scientists, the missile is noteworthy for looking beyond past achievements that had used German ideas. For example, instead of using jet vanes for control, which increased resistance generated at the engine nozzle exhaust outlet, the R-7 used special control engines. These same engines served as the last stage’s vernier thrusters.[3]

Because of clustered design, each booster had its own propellant tanks. The design team had to develop a system to regulate the propellant component consumption ratio and to synchronize the consumption between the boosters.[3]

Starting from the R-1, which was a copy of the German V-2, a free-standing missile was launched from a horizontal pad. It turned out that assembling a cluster of a central core and four boosters on the pad is almost impossible without it falling apart. Also, a wind gust could knock the missile off of the pad. The solution was to eliminate the pad and to suspend the entire rocket in the trusses that bear both vertical weight load as well as horizontal wind forces. The launch system simulated flight conditions with strap-on boosters pushing the central core forward.[3]

The new missile's GRAU index was 8K71. The first flight ready vehicle was delivered to Baikonour Cosmodrome on 1 May and flown on the 15th. A fire broke out in the Blok D strap-on almost immediately at liftoff. It broke away from the booster at T+88 seconds, which crashed 400 km (248 miles) downrange. The next attempt on 11 June (notable the same day the United States conducted its first test launch of an ICBM), an electrical short caused the missile to start rolling uncontrollably and disintegrate 33 seconds after liftoff. The first successful long flight, of 6,000 km (3,700 mi), was made on 21 August 1957. The dummy warhead impacted in the Pacific Ocean and five days later, TASS announced that the Soviet Union had "successfully tested a multi-stage intercontinental ballistic missile". A modified version of the missile (8K71PS) placed Sputnik 1 in orbit from Baikonur on 4 October 1957 and Sputnik 2 on 3 November 1957.

The next ICBM test took place on 30 January 1958, but the strap-ons failed to separate cleanly and damaged plumbing in the core stage, which lost thrust and impacted far off target. These early flights revealed assorted design flaws in the R-7 which necessitated multiple modifications to the missile. Testing continued through December 1959, and the last original 8K71 flew on 27 February 1961. The additional development resulted in the 8K74 (also known as R-7A), which was lighter, had better navigation systems, more powerful engines, extended its range to 12,000 km by carrying more fuel, and increased payload to 5,370 kg (11,840 lb). In addition, the missile was designed to be easier to take apart and service. The warhead was tested on Novaya Zemlya in October 1957 and again in 1958, yielding an estimated 2.9 Mt. Aside from the initial Sputnik launches, the 8K71 formed the basis of the 8K72 booster used for the first generation Luna probes. However, six out of nine Luna probes launched on the 8K72 failed. Combined with the failed Sputnik launch on 27 April 1958, this brought the booster's total space launch record to 6 successes in 13 attempts. The improved 8K74 would then form the basis for the later Vostok and Molniya boosters, greatly increasing reliability.

Operational history

The first strategic-missile unit became operational on 9 February 1959 at Plesetsk in north-west Russia.[4] On 15 December 1959 the R-7 missile was tested at Plesetsk for the first time. The missiles were fully deployed by 1962.

Total service was limited to no more than ten nuclear armed missiles active at any time. A single launch pad was operational at Baikonur and from six to eight were in operation at Plesetsk.[5]

The costs of the system were high, mostly due to the difficulty of constructing in remote areas the large launch sites required. At one point, each launch site was projected to cost 5% of the total Soviet defense budget. However, these huge costs were not unique for a first generation missile and the US experienced similar problems.

Besides the cost, the missile system faced other operational challenges. With the U-2 overflights, the huge R-7 launch complexes could not be hidden and therefore could be expected to be destroyed quickly in any nuclear war. Also, the R-7 took almost twenty hours to prepare for launching, and it could not be left on alert for more than a day due to its cryogenic fuel system. Therefore, the Soviet force could not be kept on permanent alert, and could have been subject to an air strike before launching. Additionally the huge payload for which it was designed, adapted to early heavy H-bombs, became irrelevant with the coming of lighter bomb technology.

The limitations of the R-7 pushed the Soviet Union into rapidly developing second-generation missiles which would be more viable weapons systems. The R-7 was phased out of military service by 1968.

While the R-7 turned out to be impractical as a weapon, it became the basis for a series of Soviet expendable space launch vehicles. The derivatives of the R-7 missile became successful space launch vehicles, which are still being used in modified form.

Variants

SS-6 Sapwood
NATO reporting name for all versions of the R-7, variants identified by suffix letter on the name portion (e.g. Sapwood-A).
R-7 Semyorka
First launch 15 May 1957, last launch 27 February 1961; 27 launch attempts, 18 of which were successful.
R-7A Semyorka
First launch 23 December 1959, last launch 25 July 1967; 21 launch attempts, 18 of which were successful.
8K71
The GRAU designation for the R-7 Semyorka missile (GRAU 8K: Missiles 71: model number)
8K74
The GRAU designation for the R-7A Semyorka missile (GRAU 8K: Missiles 74: model number)
8K71PS
Sputnik 1 launcher Soyuz-FG (11A511U-FG) and

Note: Much developed variants of the R-7 are still active:

Operators

 Soviet Union
The Strategic Missile Troops was the only operator of the Semyorka.

See also

References

  1. ↑ Wade, Mark. "R-7". Encyclopedia Astronautica. Retrieved 4 July 2011.
  2. ↑ "Rocket R-7". S.P.Korolev RSC Energia.
  3. 1 2 3 "Boris Chertok: Rockets and People, p. 290" (PDF). Archived from the original (PDF) on 2008-05-11.
  4. ↑ "This Week in EUCOM History: February 6–12, 1959". EUCOM. 6 February 2012. Retrieved 8 February 2012.
  5. ↑
  • The Kremlin's Nuclear Sword, Steven J. Zaloga, Smithsonian Institution Press, Washington and London, 2002.

External links

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