Sputnik rocket

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Sputnik (8K71PS/8A91)
Sputnik rocket
Sputnik rocket
Fact sheet
Function Small carrier rocket
Manufacturer OKB-1
Country of origin Flag of the Soviet Union Soviet Union
Size
Height 8K71PS: 30.0 m (98 ft)
8A91: 31.1 m (102 ft)
Diameter 2.99 m (9.8 ft)
Mass 267,000 kg (590,000 lb)
8A91: 269,300 kg (594,000 lb)
Stages 1
Capacity
Payload to
LEO (8K71PS)
8K71PS: 500 kg (1,100 lb)
8A91: 1,327 kg (2,930 lb)
Associated Rockets
Family R-7
Comparable Vanguard
Juno I
Launch History
Status Retired
Launch sites LC-1/5, Baikonur
Total launches 4 (2 8K71PS, 2 8A91)
Successes 3
Failures 1 (8A91)
Maiden flight 8K71PS: 4 October 1957
8A91: 27 April 1958
Last flight 8K71PS: 3 November 1957
8A91: 15 May 1958
Notable payloads Sputnik 1
Sputnik 2
Sputnik 3
Boosters (Stage 0)
No boosters 4
Engines 1 RD-107
Thrust 970 kN (220,000 lbf)
Specific impulse 306 sec
Burn time 120 seconds
Fuel LOX/RP-1
First Stage
Engines 1 RD-108
Thrust 912 kN (205,000 lbf)
Specific impulse 308 sec
Burn time 330 seconds
Fuel LOX/RP-1

The Sputnik rocket was an unmanned orbital carrier rocket designed by Sergey Korolyov, derived from the R-7 Semyorka ICBM. On 4 October 1957, it was used to perform the world's first satellite launch, placing Sputnik 1 into a low Earth orbit.

Two versions of the Sputnik were built, the Sputnik-PS (GRAU index 8K71PS), which was used to launch Sputnik 1 and later Sputnik 2, and the Sputnik (8A91), which failed to launch a satellite in April 1958, and subsequently launched Sputnik 3 on 15 May 1958.

A later member of the R-7 family, the Polyot, used the same configuration as the Sputnik rocket, but was constructed from Voskhod components. Because of the similarity, the Polyot was sometimes known as the Sputnik 11A59.