RD-0124
Chemical Automatics Design Bureau (KBKhA) RD-0124, also designated 14D23, is a four-chamber oxidizer-rich staged-combustion liquid-oxygen/kerosene engine for the third stage of Soyuz-2.1b, Soyuz-2.1v, and Soyuz-STB. KBKhA reports 30 metric-ton-force (approximately 294.2 kN) vacuum thrust, 359 s vacuum specific impulse, and 300 s main-mode operation; it records first flight in 2006 and continuing commercial deliveries.
Identity
- Aliases
- RD-0124RD012414D2314Д23KBKhA RD-0124
- Domains
- spaceflight
- Identity Level
- model
- Kind
- liquid-rocket-engine
- Name
- RD-0124
- Status
- active
Details
- Description
- Chemical Automatics Design Bureau (KBKhA) RD-0124, also designated 14D23, is a four-chamber oxidizer-rich staged-combustion liquid-oxygen/kerosene engine for the third stage of Soyuz-2.1b, Soyuz-2.1v, and Soyuz-STB. KBKhA reports 30 metric-ton-force (approximately 294.2 kN) vacuum thrust, 359 s vacuum specific impulse, and 300 s main-mode operation; it records first flight in 2006 and continuing commercial deliveries.
- Developers
- Manufacturers
- Propellants
- keroseneliquid oxygen
- Rocket Specs
- Burn Time S
- 300
- Chamber Count
- 4
- Cycle
- oxidizer-rich staged combustion
- Vacuum Specific Impulse S
- 359
- Vacuum Thrust Kn
- 294.2
Links
Assets & Meta
- Creation Time
- July 29, 2026 at 11:38:47 UTC
- Updated Time
- August 22, 2026 at 07:40:56 UTC
Other
- Sources
- Accessed Date
- 2026-07-29
- Publisher
- Chemical Automatics Design Bureau (KBKhA)
- Title
- RD0124