RD-214

The RD-214 (GRAU Index 8D59) was a liquid rocket engine, burning AK-27I (a mixture of 73% nitric acid and 27% N₂O₄ + iodine passivant and TM-185 (a kerosene and gasoline mix) in the gas generator cycle. As was the case with many V-2 influenced engines, the single turbine was driven by steam generated by catalytic decomposition of hydrogen peroxide. It also had four combustion chambers and vector control was achieved by refractory vanes protruding into the nozzle's exhaust.

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Location: KML, Cluster Map, Maps,

Frameless

Strategic Missile Forces Museum - missile R-12

RD-214 rocket engine

RD-214 cuted chamber

Двигатель РД-214 - Музей космонавтики и ракетной техники

Rd 214

Type	Subtype	Date	Description	Notes	Source
commons	image		Strategic Missile Forces Museum - missile R-12		Commons
commons	image		RD-214 rocket engine		Commons
commons	image		RD-214 cuted chamber		Commons
commons	image		Двигатель РД-214 - Музей космонавтики и ракетной техники		Commons
commons	image		Rd 214		Commons