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AKA: 11D55; 8D715K; 8D715P; RD-461; RD-461, 11D55, 8D715K, RO-8; RO-8. Date: 1961-65. Number: 326 . 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. Launch Vehicles: Molniya 8K78, Voskhod 11A57. Propellants: Lox/Kerosene. Stages: Molniya 8K78-2, Voskhod 11A57-2. Agency: Kosberg bureau. More at: 7465. Bibliography: 177. 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 � 1997-2016 Mark Wade - Contact � / Conditions for Use |
