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The RD-120 (Russian: Ракетный Двигатель-120, romanized: Raketnyy Dvigatel-120, lit. 'Rocket Engine 120', GRAU index: 11D123) is a liquid upper stage rocket engine burning RG-1 (refined kerosene) and LOX in an oxidizer rich staged combustion cycle with an O/F ratio of 2.6. It is used in the second stage of the Zenit family of launch vehicles. It has a…
History, Technological derivatives & Overview
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engine stage npo energomash second development combustion zenit first launch engines version lox family staged rd-810 yuzhmash project program kerosene
| Subject | Predicate | Object | Confidence | Src |
|---|---|---|---|---|
| RD-120 | Application | Upper stage | 1.00 | infobox |
| RD-120 | Burn time | 315 seconds | 1.00 | infobox |
| RD-120 | Chamber pressure | Standard: 162.8 bar (16.28 MPa) Uprated: 178.1 bar (17.81 MPa) | 1.00 | infobox |
| RD-120 | Country of origin | Soviet Union | 1.00 | infobox |
| RD-120 | Country of origin | Russia | 1.00 | infobox |
| RD-120 | Cycle | Staged combustion cycle | 1.00 | infobox |
| RD-120 | Designer | NPO Energomash, V.K.Chvanov, V.P. Radovsky | 1.00 | infobox |
| RD-120 | Diameter | 1.95 m (6.4 ft) | 1.00 | infobox |
| RD-120 | Dry mass | 1,125 kg (2,480 lb) | 1.00 | infobox |
| RD-120 | Length | 3.87 m (12.7 ft) | 1.00 | infobox |
| RD-120 | Manufacturer | Yuzhmash | 1.00 | infobox |
| RD-120 | Propellant | LOX / RP-1 | 1.00 | infobox |
| RD-120 | Specific impulse, vacuum | 350 s (3.4 km/s) | 1.00 | infobox |
| RD-120 | Status | Operational | 1.00 | infobox |
| RD-120 | Thrust, vacuum | Standard: 834 kN (187,000 lbf) Uprated: 912 kN (205,000 lbf) | 1.00 | infobox |
| RD-120 | Thrust-to-weight ratio | Standard: 75.55[note 1] Uprated: 82.66[note 2] | 1.00 | infobox |
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