RD-0212

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RD-0212

Part of RD-0202

RD-0212
CADB Museum, March 1992.
Credit: © Dietrich Haeseler

Kosberg N2O4/UDMH rocket engine. Proton stage 3. Engine unit consisting of 1 RD-0213 main engine and 4 RD-0214 vernier/steering engines. 8D48 essentially similar to 8D411 and 8D412 and has the same combustion chamber. First flight 1967.

AKA: 8D49;RD-473. Date: 1962-68. Number: 306 . Thrust: 613.00 kN (137,807 lbf). Specific impulse: 325 s. Burn time: 230 s.

Chambers: 1 + 4.

Family: Storable liquid. Country: Russia. Launch Vehicles: Monoblock UR-500, Polyblock UR-500, Proton-K, Proton-K/D, Proton-K/DM, Proton-K/D-1, Proton-K/DM-2, Proton-K/DM-2 DM1, Proton-K/D-2, Proton-K/DM-2M, Proton-K/17S40, Proton-K/17S40 DM2. Propellants: N2O4/UDMH. Stages: Monoblock UR-500-3, Proton K-3, Proton M-3. Agency: Kosberg bureau. Bibliography: 307, 7481.

Photo Gallery

RD-0212
Credit: KBKhA

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