Back to Propulsion Systems

NK-43

UEC-Kuznetsov NK-43 tested upper-stage LOX/kerosene liquid rocket engine, an oxygen-rich staged-combustion modification of NK-15V developed for the N1 second stage. NASA records about 395,000 lbf (about 1,757 kN) vacuum thrust and restart capability; UEC distinguishes the NK-43 second-stage boundary from the NK-33 first-stage engine. Historical status is preserved and no flight installation is asserted.

Identity

Aliases
NK-43Kuznetsov NK-43N1 second-stage NK-43UEC NK-43
Domains
spaceflight
Identity Level
variant
Kind
liquid-rocket-engine
Name
NK-43
Status
historical

Details

Description
UEC-Kuznetsov NK-43 tested upper-stage LOX/kerosene liquid rocket engine, an oxygen-rich staged-combustion modification of NK-15V developed for the N1 second stage. NASA records about 395,000 lbf (about 1,757 kN) vacuum thrust and restart capability; UEC distinguishes the NK-43 second-stage boundary from the NK-33 first-stage engine. Historical status is preserved and no flight installation is asserted.
Developers
Lineage
Manufacturers
Propellants
keroseneliquid oxygen
Rocket Specs
Cycle
oxygen-rich staged combustion
Restartable
Yes
Vacuum Thrust Kn
1,757

Links

Assets & Meta

Creation Time
July 29, 2026 at 11:49:28 UTC
Updated Time
August 22, 2026 at 07:52:29 UTC

Other

Sources