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The RD-107 (Russian: Ракетный Двигатель-107, romanized: Raketnyy Dvigatel-107, lit. 'Rocket Engine 107') and its sibling, the RD-108, are a type of rocket engine used on the R-7 rocket family. RD-107 engines are used in each booster and the RD-108 is used in the central core. The engines have four main combustion chambers (each with a nozzle) and either…
Versions, Design & Production
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| Subject | Predicate | Object | Confidence | Src |
|---|---|---|---|---|
| RD-107 | Application | Booster/first stage | 1.00 | infobox |
| RD-107 | Associated LV | R-7 family | 1.00 | infobox |
| RD-107 | Country of origin | Soviet Union | 1.00 | infobox |
| RD-107 | Country of origin | Russia | 1.00 | infobox |
| RD-107 | Cycle | Gas-generator | 1.00 | infobox |
| RD-107 | Designer | OKB-456 | 1.00 | infobox |
| RD-107 | Dry mass | 1,190 kg (2,620 lb) | 1.00 | infobox |
| RD-107 | Manufacturer | JSC Kuznetsov | 1.00 | infobox |
| RD-107 | Notes | Performance figures are for RD-107A | 1.00 | infobox |
| RD-107 | Predecessor | RD-105 | 1.00 | infobox |
| RD-107 | Propellant | LOX / RG-1 | 1.00 | infobox |
| RD-107 | Specific impulse, sea-level | 263.3 s (2.582 km/s) | 1.00 | infobox |
| RD-107 | Specific impulse, vacuum | 320.2 s (3.140 km/s) | 1.00 | infobox |
| RD-107 | Status | In production | 1.00 | infobox |
| RD-107 | Thrust, sea-level | 839 kN (189,000 lbf) | 1.00 | infobox |
| RD-107 | Thrust, vacuum | 1,020 kN (230,000 lbf) | 1.00 | infobox |
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