R6-117

Engine · Russia

Original archive entry. The text, images and links below are kept as they were written.

Chelomei N2O4/UDMH rocket engine. LK-1 Blok A. Developed 1964-66. Developed in cooperation with OKB-117 on the basis of the latter's main engine for the UR-100 stage II.

Family: Storable liquid
Country: Russia
Spacecraft: LK-1
Propellants: N2O4/UDMH
Agency: Chelomei bureau

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