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The Angara (Ангара) is a family of launch vehicles being developed by the Moscow-based Khrunichev State Research and Production Space Center. The launch vehicles are to put between 3,800 kg (8,400 lb) and 24,500 kg (54,000 lb) into low Earth orbit and are intended, along with Soyuz-2 variants, to replace several existing launch vehicles.
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angara stage launch urm-1 flight a5 first khrunichev vehicle would second upper rd-191 boosters engine core orbit plesetsk also powered
| Subject | Predicate | Object | Confidence | Src |
|---|---|---|---|---|
| Angara (rocket family) | Burn time | 214 seconds | 1.00 | infobox |
| Angara (rocket family) | Burn time | Angara 1.2: 214 seconds Angara A5: 325 seconds | 1.00 | infobox |
| Angara (rocket family) | Burn time | 424 seconds | 1.00 | infobox |
| Angara (rocket family) | Burn time | 3,000 seconds | 1.00 | infobox |
| Angara (rocket family) | Burn time | 1,350 seconds | 1.00 | infobox |
| Angara (rocket family) | Comparable | Naro-1 used a modified URM-1 first stage | 1.00 | infobox |
| Angara (rocket family) | Cost per launch | A5: US$100 million (2021) | 1.00 | infobox |
| Angara (rocket family) | Country of origin | Russia | 1.00 | infobox |
| Angara (rocket family) | Derivative work | A1.2pp | 1.00 | infobox |
| Angara (rocket family) | Derivative work | A1.2 | 1.00 | infobox |
| Angara (rocket family) | Derivative work | A5 | 1.00 | infobox |
| Angara (rocket family) | First flight | A1.2pp: 9 July 2014 A1.2: 29 April 2022 A5: 23 December 2014 | 1.00 | infobox |
| Angara (rocket family) | Function | Launch vehicle | 1.00 | infobox |
| Angara (rocket family) | Height | 42.7–64 m (140–210 ft) | 1.00 | infobox |
| Angara (rocket family) | Last flight | A1.2: 23 April 2026 (most recent) | 1.00 | infobox |
| Angara (rocket family) | Last flight | A5: 19 June 2025 (most recent) | 1.00 | infobox |
| Angara (rocket family) | Launch sites | Plesetsk, Site 35/1 Vostochny, Site 1A | 1.00 | infobox |
| Angara (rocket family) | Manufacturer | Khrunichev · KBKhA | 1.00 | infobox |
| Angara (rocket family) | Mass | 171,500–790,000 kg (378,100–1,741,700 lb) | 1.00 | infobox |
| Angara (rocket family) | Mass | 3,800–24,500 kg (8,400–54,000 lb) | 1.00 | infobox |
| Angara (rocket family) | Mass | 5,400–7,500 kg (11,900–16,500 lb) | 1.00 | infobox |
| Angara (rocket family) | Maximum thrust | 1,920 kN (430,000 lbf) | 1.00 | infobox |
| Angara (rocket family) | Maximum thrust | 294.3 kN (66,200 lbf) | 1.00 | infobox |
| Angara (rocket family) | Maximum thrust | 19.6 kN (4,400 lbf) | 1.00 | infobox |
| Angara (rocket family) | Maximum thrust | 68.6 kN (15,400 lbf) | 1.00 | infobox |
| Angara (rocket family) | No. boosters | 4 | 1.00 | infobox |
| Angara (rocket family) | Partial failure | 1 (A5: 1) | 1.00 | infobox |
| Angara (rocket family) | Powered by | 1 × RD-191 | 1.00 | infobox |
| Angara (rocket family) | Powered by | 1 × RD-0124A | 1.00 | infobox |
| Angara (rocket family) | Powered by | 1 × S5.98M | 1.00 | infobox |
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