Back to Propulsion Systems

RD-0124A

KBKhA four-chamber LOX/kerosene staged-combustion upper-stage engine for Angara. RD-0124A derives from RD-0124 but changes fuel extraction for chamber-deflection control, tank pressurization, and flight duration; KBKhA records 30 tf vacuum thrust, 359 s vacuum specific impulse, successful Angara 1.2PP and Angara-5 flight tests, and continuing manufacture for Angara. Lifecycle remains active based on repeated flight operation and current production evidence.

Identity

Domains
spaceflight
Identity Level
variant
Kind
liquid-rocket-engine
Name
RD-0124A
Status
active

Details

Description
KBKhA four-chamber LOX/kerosene staged-combustion upper-stage engine for Angara. RD-0124A derives from RD-0124 but changes fuel extraction for chamber-deflection control, tank pressurization, and flight duration; KBKhA records 30 tf vacuum thrust, 359 s vacuum specific impulse, successful Angara 1.2PP and Angara-5 flight tests, and continuing manufacture for Angara. Lifecycle remains active based on repeated flight operation and current production evidence.
Developers
Lineage
Manufacturers
Propellants
keroseneliquid oxygen
Rocket Specs
Chamber Count
4
Vacuum Specific Impulse S
359
Vacuum Thrust Kn
294.2

Links

Assets & Meta

Creation Time
July 29, 2026 at 11:38:53 UTC
Updated Time
August 15, 2026 at 04:10:51 UTC

Other

Sources