hat
kòz aksidan an fèt la te mank algoritm kontwòl misil ak etap la anwo. Lè ekspoze kòrèk premye azimit “Inyon” ak “bato” algorithm pèfòmans sistèm kontwòl a nan la, ke apre, kòm sèn nan anwo separe de misil yo te pase nominal, Oryantasyon li yo te idantifye mal.
eng
cause of the accident was inadequate missile control algorithms and the upper stage. When exposed incorrect initial azimuth “Union” and “frigate” Control system performance algorithm resulted in the, that after, as the upper stage separated from the spent missiles nominally, its orientation was identified incorrectly.