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RD-0214


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A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z 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. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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