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RD-0125A

KBKhA single-chamber LOX/naphthyl liquid-rocket engine derived from the four-chamber RD-0124A for a proposed Angara-A5 third-stage upgrade. KBKhA publishes 29.5 tf vacuum thrust, 353 s vacuum specific impulse and 160 kgf/cm² chamber pressure; work is paused at the technical-project stage, so no flight or active-service status is asserted.

Identity

Aliases
RD-0125ARD0125AKBKhA RD-0125AAngara-A5 third-stage RD-0125A
Domains
spaceflight
Identity Level
variant
Kind
liquid-rocket-engine
Name
RD-0125A
Status
development

Details

Description
KBKhA single-chamber LOX/naphthyl liquid-rocket engine derived from the four-chamber RD-0124A for a proposed Angara-A5 third-stage upgrade. KBKhA publishes 29.5 tf vacuum thrust, 353 s vacuum specific impulse and 160 kgf/cm² chamber pressure; work is paused at the technical-project stage, so no flight or active-service status is asserted.
Developers
Lineage
  • Note
    KBKhA identifies RD-0125A as a single-chamber LOX/naphthyl engine derived from the four-chamber RD-0124A for a proposed Angara-A5 third-stage upgrade; work is paused at the technical-project stage.
    Related Propulsion System
    Relationship
    direct-derivative-of
    Sources
Manufacturers
Propellants
liquid oxygennaphthyl
Rocket Specs
Chamber Count
1
Vacuum Specific Impulse
…
Vacuum Thrust
…

Links

Assets & Meta

Creation Time
August 15, 2026 at 04:12:54 UTC
Updated Time
August 22, 2026 at 08:20:13 UTC

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Sources