Soyuz (rocket)
A Soyuz rocket being rolled out to the launch pad at the Baikonur Cosmodrome in Kazakhstan. |
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| Function | Carrier rocket |
|---|---|
| Manufacturer | OKB-1 |
| Country of origin | |
| Size | |
| Height | 45.6 metres (150 ft) |
| Diameter | 10.3 metres (34 ft) |
| Mass | 308,000 kilograms (680,000 lb) |
| Stages | 2 |
| Capacity | |
| Payload to LEO |
6,450 kilograms (14,200 lb) |
| Associated rockets | |
| Family | R-7 |
| Derivatives | Soyuz-U Soyuz-U2 Soyuz-FG Soyuz-2 |
| Launch history | |
| Status | Retired |
| Launch sites | Baikonur Sites 1/5 & 31/6 |
| Total launches | 30 |
| Successes | 28 |
| Failures | 2 |
| First flight | 28 November 1966 |
| Last flight | 24 May 1975 |
| Notable payloads | Soyuz |
| Boosters (Stage 0) - Block A/B/V/G | |
| No boosters | 4 |
| Engines | 1 RD-107 |
| Thrust | 994.3 kilonewtons (223,500 lbf) |
| Specific impulse | 315 sec |
| Burn time | 118 seconds |
| Fuel | RP-1/LOX |
| First Stage - 11S59 | |
| Engines | 1 RD-108 |
| Thrust | 977.7 kilonewtons (219,800 lbf) |
| Specific impulse | 315 sec |
| Burn time | 292 seconds |
| Fuel | RP-1/LOX |
| Second Stage - 11S510 | |
| Engines | 1 RD-0110 |
| Thrust | 294 kilonewtons (66,000 lbf) |
| Specific impulse | 330 sec |
| Burn time | 246 seconds |
| Fuel | RP-1/LOX |
The Soyuz (Russian: Союз, meaning "union", GRAU index 11A511) was a Soviet expendable carrier rocket designed by OKB-1 and manufactured by State Aviation Plant No. 1 in Samara, Russia. It was used to launch Soyuz spacecraft as part of the Soyuz programme, initially on unmanned test flights, followed by the first 19 manned launches of the programme.[1]
The 11A511 first flew in 1966, and was derived from the Voskhod 11A57 rocket, but introduced a new, uprated core stage and strap-ons, which became standard for all R-7 derived launch vehicles to replace the numerous older variants in use on the 8A92, 11A57, and 8K78M.[2] it was a member of the R-7 family of rockets. It was a two-stage rocket, with four liquid-fuelled strap-on boosters clustered around the first stage, with a Block I second stage.
The aborted Soyuz 18-1 launch in 1975 was the final manned flight of the 11A511 and as it occurred shortly before the ASTP mission, the United States requested that the Soviets provide details about this failure. They stated that Soyuz 19 would be using a newer model of booster (ie. the 11A511U) and Soyuz 18-1's malfunction had no bearing on it.
Soyuz rockets are assembled horizontally in the MIK Building at the launch site. The rocket is then rolled out, and erected on the launch pad.
References [edit]
| Wikimedia Commons has media related to: Soyuz (rocket) |
- ^ Wade, Mark. "Soyuz". Encyclopedia Astronautica. Retrieved 2009-04-16.
- ^ ""Soyuz" - series launch vehicles". Samara Space Centre.
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