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.