R6-117
Designer: Chelomei. Developed in: 1964-66. Application: LK-1 Blok A. Propellants: N2O4/UDMH. Thrust(vac): 132.000 kN (29,674 lbf). Country: Russia. Status: Developed 1964-66.

Developed in cooperation with OKB-117 on the basis of the latter's main engine for the UR-100 stage II.

R6-117 used on Spacecraft

 
 
 
 
 
 
 
 
 
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