![]() Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9 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-0206 AKA: 8D47. Status: Developed 1961-64. Date: 1961-64. Thrust: 575.50 kN (129,378 lbf). Specific impulse: 326 s. Burn time: 150 s. Diameter: 1.47 m (4.82 ft).
Chamber Pressure: 147.00 bar. Area Ratio: 81.3. Oxidizer to Fuel Ratio: 2.6.
Family: Storable liquid. Country: Russia. Propellants: N2O4/UDMH. Stages: UR-200-2. Agency: Kosberg bureau. Bibliography: 309, 320, 7475. Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9 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 © 1997-2017 Mark Wade - Contact © / Conditions for Use |