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The Soyuz (Russian: Союз, meaning "union", GRAU index 11A511, Sheldon: A-2, DoD: SL-4) was a Soviet expendable carrier rocket designed in the 1960s by OKB-1 and manufactured by State Aviation Plant No. 1 in Kuybyshev, Soviet Union. It was commissioned to launch Soyuz spacecraft as part of the Soviet human spaceflight program, first with eight uncrewed…
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soyuz launch soviet 11a511 booster rocket launches r-7 soyuz-u flights also years 8k78m variants avd would shutdown union first flight
| Subject | Predicate | Object | Confidence | Src |
|---|---|---|---|---|
| Soyuz (rocket) | Burn time | 118 seconds | 1.00 | infobox |
| Soyuz (rocket) | Burn time | 292 seconds | 1.00 | infobox |
| Soyuz (rocket) | Burn time | 246 seconds | 1.00 | infobox |
| Soyuz (rocket) | Carries passengers or cargo | Soyuz | 1.00 | infobox |
| Soyuz (rocket) | Country of origin | Soviet Union | 1.00 | infobox |
| Soyuz (rocket) | Derivative work | Soyuz-L | 1.00 | infobox |
| Soyuz (rocket) | Derivative work | Soyuz-M | 1.00 | infobox |
| Soyuz (rocket) | Derivative work | Soyuz-U | 1.00 | infobox |
| Soyuz (rocket) | Diameter | 10.3 m (33 ft 10 in) | 1.00 | infobox |
| Soyuz (rocket) | Failure(s) | 2 (Soyuz 7K-OK No.1 & Soyuz 18a) | 1.00 | infobox |
| Soyuz (rocket) | Family | R-7 (Soyuz) | 1.00 | infobox |
| Soyuz (rocket) | First flight | 28 November 1966 (Kosmos 133) | 1.00 | infobox |
| Soyuz (rocket) | Function | Medium-lift launch vehicle | 1.00 | infobox |
| Soyuz (rocket) | Height | 50.7 m (166 ft 4 in) | 1.00 | infobox |
| Soyuz (rocket) | Last flight | 14 October 1976 (Soyuz 23) | 1.00 | infobox |
| Soyuz (rocket) | Launch sites | Baikonur, Sites 1/5 & 31/6 | 1.00 | infobox |
| Soyuz (rocket) | Manufacturer | OKB-1 | 1.00 | infobox |
| Soyuz (rocket) | Mass | 308,000 kg (679,000 lb) | 1.00 | infobox |
| Soyuz (rocket) | Mass | 6,450 kg (14,220 lb) | 1.00 | infobox |
| Soyuz (rocket) | Maximum thrust | SL: 755.14 kN (169,760 lbf) | 1.00 | infobox |
| Soyuz (rocket) | Maximum thrust | vac: 921.86 kN (207,240 lbf) | 1.00 | infobox |
| Soyuz (rocket) | Maximum thrust | SL: 676.68 kN (152,120 lbf) | 1.00 | infobox |
| Soyuz (rocket) | Maximum thrust | vac: 833.60 kN (187,400 lbf) | 1.00 | infobox |
| Soyuz (rocket) | Maximum thrust | 294 kN (66,000 lbf) | 1.00 | infobox |
| Soyuz (rocket) | No. boosters | 4 | 1.00 | infobox |
| Soyuz (rocket) | Powered by | 1 × RD-107MM | 1.00 | infobox |
| Soyuz (rocket) | Powered by | 1 × RD-108MM | 1.00 | infobox |
| Soyuz (rocket) | Powered by | 1 × RD-0110 | 1.00 | infobox |
| Soyuz (rocket) | Propellant | LOX / RG-1 | 1.00 | infobox |
| Soyuz (rocket) | Specific impulse | SL: 257 s (2.52 km/s) | 1.00 | infobox |
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