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This rocket article contains payload capacity, but does not include orbital altitude or inclination , which greatly affects the capacity. |
Function | Interim carrier rocket |
---|---|
Manufacturer | OKB-1 |
Country of origin | Soviet Union |
Size | |
Stages | Three |
Capacity | |
Payload to LEO | |
Mass | 4,500 kilograms (9,900 lb) |
Associated rockets | |
Family | R-7 |
Launch history | |
Status | Retired |
Launch sites | Baikonur 31/6 |
Total launches | 2 |
Success(es) | 2 |
First flight | 27 December 1965 |
Last flight | 20 July 1966 |
People or cargo transported | US-A |
Boosters – Block A/B/V/G | |
No. boosters | 4 |
Powered by | 1 RD-107 |
Maximum thrust | 994.3 kilonewtons (223,500 lbf) |
Specific impulse | 315 sec |
Burn time | 118 seconds |
Propellant | RP-1/LOX |
First stage –11S59 | |
Powered by | 1 RD-108 |
Maximum thrust | 977.7 kilonewtons (219,800 lbf) |
Specific impulse | 315 sec |
Burn time | 292 seconds |
Propellant | RP-1/LOX |
Second stage | |
Powered by | 1 RD-0109 |
Maximum thrust | 54.5 kN |
Burn time | 365 seconds |
Propellant | RP-1/LOX |
Third stage –Unknown | |
The Soyuz/Vostok,also known as just Soyuz or Vostok,or by its GRAU index,11A510 was an interim expendable carrier rocket used by the Soviet Union in 1965 and 1966. Two were launched with prototype US-A satellites. [1]
The Soyuz/Vostok was launched from Site 31/6 at the Baikonur Cosmodrome. It consisted of the first stage and boosters from a Soyuz rocket combined with the second stage of the Vostok-2,and an unknown third stage. [1] Along with the Voskhod-derived Polyot,it was built as an interim between the cancellation of the UR-200 development programme,and the introduction of the Tsyklon-2,which took over US-A launches once it entered service.
The Space Race was a 20th-century competition between two Cold War adversaries,the Soviet Union and the United States,to achieve superior spaceflight capability. It had its origins in the ballistic missile-based nuclear arms race between the two nations following World War II. The technological advantage demonstrated by spaceflight achievement was seen as necessary for national security,and became part of the symbolism and ideology of the time. The Space Race brought pioneering launches of artificial satellites,robotic space probes to the Moon,Venus,and Mars,and human spaceflight in low Earth orbit and ultimately to the Moon.
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Plesetsk Cosmodrome is a Russian spaceport located in Mirny,Arkhangelsk Oblast,about 800 km north of Moscow and approximately 200 km south of Arkhangelsk,the cosmodrome dates from 1957. Originally developed as an ICBM site for the R-7 missile,it also served for numerous satellite launches using the R-7 and other rockets. Its high latitude makes it useful only for certain types of launches,especially the Molniya orbits,so for much of the site's history it functioned as a secondary location,with most orbital launches taking place from Baikonur,in the Kazakh SSR. With the end of the Soviet Union,Baikonur became a foreign territory,and Kazakhstan charged $115 million usage fees annually. Consequently,Plesetsk has seen considerably more activity since the 2000s.
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Vostok was a family of rockets derived from the Soviet R-7 Semyorka ICBM and was designed for the human spaceflight programme. This family of rockets launched the first artificial satellite and the first crewed spacecraft (Vostok) in human history. It was a subset of the R-7 family of rockets.
The Voskhod rocket was a derivative of the Soviet R-7 ICBM designed for the human spaceflight programme but later used for launching Zenit reconnaissance satellites. It consisted of the Molniya 8K78M third stage minus the Blok L. In 1966,all R-7 variants were equipped with the uprated core stage and strap-ons of the Soyuz 11A511. The Blok I stage in the Voskhod booster used the RD-0107 engine rather than the crew rated and more powerful RD-0110 used on the Soyuz. The sole exception to this were the two manned Voskhod launches,which had RD-0108 engines,a crew-rated RD-0107 but with the same performance.
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