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 H2O2. It also had four combustion chambers and vector control was achieved by refractory vanes protruding into the nozzles exhaust.
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 H2O2. It also had four combustion chambers and vector control was achieved by refractory vanes protruding into the nozzles exhaust.
has abstract
RD-214 – silnik rakietowy kons ...... okonywany był mieszanką TG-02.
@pl
RD-214(ロシア語: РД-214、GRAU認識番号8D ...... 様に燃焼室と推力偏向はノズルの排気を偏流翼によって偏向する。
@ja
The RD-214 (GRAU Index 8D59) w ...... ding into the nozzles exhaust.
@en
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Wikipage page ID
47,105,558
Wikipage revision ID
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associated
R-12 and Kosmos-2
burn time
Caption
Museum of Space and Missile Technology . RD-214 rocket engine for Сosmos LV first stage.
combustion chamber
country of Origin
designer
fuel
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mixture ratio
nozzle ratio
oxidiser
used in
R-12 and Kosmos-2
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comment
RD-214 – silnik rakietowy kons ...... okonywany był mieszanką TG-02.
@pl
RD-214(ロシア語: РД-214、GRAU認識番号8D ...... 様に燃焼室と推力偏向はノズルの排気を偏流翼によって偏向する。
@ja
The RD-214 (GRAU Index 8D59) w ...... ding into the nozzles exhaust.
@en
label
RD-214
@en
RD-214
@ja
RD-214
@pl