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RD-0211

Chemical Automatics Design Bureau (KBKhA) RD-0211 is a single-chamber nitrogen-tetroxide/UDMH companion engine for the Proton second stage, used as one tank-pressurization engine alongside three RD-0210 main engines. KBKhA reports 582.1 kN vacuum thrust per engine and 326.5 s vacuum specific impulse. RD-0211 was created by modernizing and redesignating RD-0209 for the three-stage Proton.

Identity

Aliases
RD-0211RD0211Proton second-stage RD-0211KBKhA RD-0211
Domains
spaceflight
Identity Level
variant
Kind
liquid-rocket-engine
Name
RD-0211
Status
active

Details

Description
Chemical Automatics Design Bureau (KBKhA) RD-0211 is a single-chamber nitrogen-tetroxide/UDMH companion engine for the Proton second stage, used as one tank-pressurization engine alongside three RD-0210 main engines. KBKhA reports 582.1 kN vacuum thrust per engine and 326.5 s vacuum specific impulse. RD-0211 was created by modernizing and redesignating RD-0209 for the three-stage Proton.
Developers
Lineage
Manufacturers
Propellants
nitrogen tetroxideUDMH
Rocket Specs
Chamber Count
1
Vacuum Specific Impulse S
326.5
Vacuum Thrust Kn
582.1

Links

Assets & Meta

Creation Time
July 29, 2026 at 11:40:25 UTC
Updated Time
August 22, 2026 at 07:51:15 UTC

Other

Sources
RD-0211 - AeroVia