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R6-117
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.

Status: Developed 1964-66. Date: 1964-66. Thrust: 132.00 kN (29,674 lbf).

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