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Rus-M (Russian: Русь-М) was a proposed launcher design which was intended to become Russia's main launch vehicle for crewed spaceflight after 2018, and an integral part of the Orel spacecraft being developed to replace the Soyuz.
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vehicle design launch stage would tsskb-progress launcher 2009 developed development rd-0146 russian payload tons version cores first rocket second roscosmos
| Subject | Predicate | Object | Confidence | Src |
|---|---|---|---|---|
| Rus-M | Country of origin | Russia | 1.00 | infobox |
| Rus-M | Diameter | 3.5 m (11 ft) (Main Core) | 1.00 | infobox |
| Rus-M | Function | Human-rated orbital launch vehicle | 1.00 | infobox |
| Rus-M | Height | 61.1 m (200 ft) | 1.00 | infobox |
| Rus-M | Launch sites | Vostochny Cosmodrome | 1.00 | infobox |
| Rus-M | Manufacturer | TsSKB-Progress | 1.00 | infobox |
| Rus-M | Mass | 233,000–1,440,000 kg (514,000–3,175,000 lb) | 1.00 | infobox |
| Rus-M | Mass | 6,500–50,000 kg (14,300–110,200 lb) | 1.00 | infobox |
| Rus-M | Maximum thrust | 4.15 MN (930,000 lbf) | 1.00 | infobox |
| Rus-M | Maximum thrust | 98.1 kN (22,100 lbf) | 1.00 | infobox |
| Rus-M | Powered by | 3 RD-180 | 1.00 | infobox |
| Rus-M | Powered by | 4 RD-0146 | 1.00 | infobox |
| Rus-M | Propellant | LOX/RP-1 | 1.00 | infobox |
| Rus-M | Propellant | LOX/LH2 | 1.00 | infobox |
| Rus-M | Specific impulse | 338 s (3.31 km/s) | 1.00 | infobox |
| Rus-M | Specific impulse | 463 s (4.54 km/s) | 1.00 | infobox |
| Rus-M | Stages | 2 - 3 | 1.00 | infobox |
| Rus-M | Status | Cancelled | 1.00 | infobox |
| Rus-M | Total launches | 0 | 1.00 | infobox |
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