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RD-0107
Part of RD-0106
RD-0110 Engine
RD-0110 Engine
Soyuz 11A511 Stage 2 engine displayed at Tsiolkovskiy Museum in Kaluga.
Credit: © Mark Wade
Kosberg LOx/Kerosene rocket engine. R-9, Molniya 8K78, Voskhod 11A57 stage 3. Out of Production. Gas generator cycle.

AKA: 8D715K;RD-461;RD-461, RO-9;RO-9. Status: Out of Production. Date: 1958-62. Thrust: 297.90 kN (66,971 lbf). Unfuelled mass: 410 kg (900 lb). Specific impulse: 326 s. Burn time: 250 s. Diameter: 0.64 m (2.09 ft).

Chambers: 4. Engine: 410 kg (900 lb). Chamber Pressure: 68.20 bar. Propellant Formulation: Lox/T-1. Thrust to Weight Ratio: 74.09.

Country: Russia. Propellants: Lox/Kerosene. Stages: Molniya 8K78-2. Agency: Kosberg bureau. Bibliography: 177, 7464.
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RD-0107RD-0107
Credit: KBKhA
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