RD-0210
The standard engine used in a three-engine set on the Proton-K and Proton-M second stage.
Identity
- Aliases
- RD-0210 / RD-0211
- Domains
- spaceflight
- Identity Level
- variant
- Kind
- liquid-rocket-engine
- Name
- RD-0210
- Status
- active
Details
- Description
- The standard engine used in a three-engine set on the Proton-K and Proton-M second stage.
- Developers
- Lineage
- Note
- KBKhA states that RD-0208 was modernized and redesignated RD-0210 for the three-stage Proton.
- Related Propulsion System
- Relationship
- direct-derivative-of
- Sources
- Nested value
- 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
- July 29, 2026 at 11:41:28 UTC
Other
- Sources
- Accessed Date
- 2026-07-29
- Publisher
- Chemical Automatics Design Bureau (KBKhA)
- Title
- Scientific and Technical Complex
- Accessed Date
- 2026-07-29
- Publisher
- Chemical Automatics Design Bureau (KBKhA)
- Title
- Three RD0210 plus one RD0211 engine block
- Accessed Date
- 2026-07-29
- Note
- Supports the legacy vehicle installation and the narrow canonical identity used for migration.
- Publisher
- Official vehicle or program source
- Title
- Proton-K official vehicle reference
- Accessed Date
- 2026-07-29
- Note
- Supports the legacy vehicle installation and the narrow canonical identity used for migration.
- Publisher
- Official vehicle or program source
- Title
- Proton-M official vehicle reference