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RD-0214
Part of RD-0207
Kosberg N2O4/UDMH rocket engine. Proton stage 3 vernier. In Production. Based on RD-0207. Four used as steering engines for Proton Stage 3 in system RD-0212. First flight 1967.

AKA: 8D811. Status: In Production. Date: 1962-68. Thrust: 30.98 kN (6,965 lbf). Specific impulse: 293 s.

Chambers: 4. Chamber Pressure: 53.00 bar.

Family: Storable liquid. Country: Russia. Propellants: N2O4/UDMH. Stages: Proton K-3. Agency: Kosberg bureau. Bibliography: 307, 7483.
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