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KBKhA RD-0213 rocket engine

RD-0213 is the main-engine component of the KBKhA RD-0212 integrated Proton third-stage propulsion block. KBKhA documents one RD-0213 paired with one RD-0214 steering engine, identifies the block nitrogen-tetroxide/UDMH propellant pair, and publishes 59.36 tonnes-force vacuum thrust and 326.5 s vacuum specific impulse for RD-0213. This component record stores those exact per-engine values while leaving standalone current lifecycle unknown.

Identity

Aliases
RD-0213RD0213RD-0213 main engine
Domains
spaceflight
Identity Level
model
Kind
liquid-rocket-engine
Name
KBKhA RD-0213 rocket engine
Status
unknown

Details

Description
RD-0213 is the main-engine component of the KBKhA RD-0212 integrated Proton third-stage propulsion block. KBKhA documents one RD-0213 paired with one RD-0214 steering engine, identifies the block nitrogen-tetroxide/UDMH propellant pair, and publishes 59.36 tonnes-force vacuum thrust and 326.5 s vacuum specific impulse for RD-0213. This component record stores those exact per-engine values while leaving standalone current lifecycle unknown.
Propellants
nitrogen tetroxideUDMH
Rocket Specs
Vacuum Specific Impulse
…
Vacuum Thrust
…

Links

Assets & Meta

Creation Time
August 15, 2026 at 05:44:19 UTC
Updated Time
August 20, 2026 at 09:36:06 UTC

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Sources