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RD-0210

Chemical Automatics Design Bureau (KBKhA) RD-0210 is a single-chamber nitrogen-tetroxide/UDMH engine for the Proton second stage, deployed as a three-engine set with one RD-0211 steering engine. KBKhA reports 59.36 metric-ton-force (approximately 582.1 kN) vacuum thrust per engine and 326.5 s vacuum specific impulse. RD-0210 was created by modernizing RD-0208 for the three-stage Proton, and serial engines were produced by Voronezh Mechanical Plant.

Identity

Aliases
RD-0210RD0210Proton second-stage RD-0210KBKhA RD-0210
Domains
spaceflight
Identity Level
variant
Kind
liquid-rocket-engine
Name
RD-0210
Status
active

Details

Description
Chemical Automatics Design Bureau (KBKhA) RD-0210 is a single-chamber nitrogen-tetroxide/UDMH engine for the Proton second stage, deployed as a three-engine set with one RD-0211 steering engine. KBKhA reports 59.36 metric-ton-force (approximately 582.1 kN) vacuum thrust per engine and 326.5 s vacuum specific impulse. RD-0210 was created by modernizing RD-0208 for the three-stage Proton, and serial engines were produced by Voronezh Mechanical Plant.
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 11:40:22 UTC
Updated Time
August 22, 2026 at 07:47:17 UTC

Other

Sources
RD-0210 - AeroVia