RD-0210
The RD-0210 (GRAU Index: 8D411K) is also known as the RD-465. It and its twin, the RD-0211, are rocket engines burning N2O4 and UDMH in an oxidizer rich staged combustion cycle. They have single nozzle, possess TVC and are the latest evolution in the RD-0203/4 lineage. They are the engines used on the Proton second stage. The RD-0213 is a fixed nozzle variation that is used on the RD-0212 module of the Proton third stage.
predecessor
primaryTopic
RD-0210
The RD-0210 (GRAU Index: 8D411K) is also known as the RD-465. It and its twin, the RD-0211, are rocket engines burning N2O4 and UDMH in an oxidizer rich staged combustion cycle. They have single nozzle, possess TVC and are the latest evolution in the RD-0203/4 lineage. They are the engines used on the Proton second stage. The RD-0213 is a fixed nozzle variation that is used on the RD-0212 module of the Proton third stage.
has abstract
The RD-0210 (GRAU Index: 8D411 ...... ule of the Proton third stage.
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Wikipage page ID
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associated
burn time
caption
Mockup
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combustion chamber
country of origin
designer
OKB-154, Yankel I. Guerchkovitch
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first date
1967-03-10
manufacturer
mixture ratio
name
RD-0210
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oxidiser
predecessor
label
RD-0210
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purpose
Upper Stage
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specific impulse vacuum
status
In Production
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type
liquid
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used in
UR-200 and UR-500 and Proton second stage
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wikiPageUsesTemplate
subject
comment
The RD-0210 (GRAU Index: 8D411 ...... ule of the Proton third stage.
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