|
RD-107-8D728
|
 | RD-107
Credit - © Mark Wade
|
Manufacturer Name: RD-107. Government Designation: 8D728. Designer: Glushko. Application: Molniya 0, Molniya 8K78M-0. Propellants: Lox/Kerosene. Thrust(vac): 996.000 kN (223,909 lbf). Thrust(sl): 818.800 kN (184,074 lbf). Isp: 314 sec. Isp (sea level): 257 sec. Burn time: 120 sec. Mass Engine: 1,145 kg (2,524 lb). Diameter: 0.67 m (2.19 ft). Length: 2.86 m (9.38 ft). Chambers: 4. Chamber Pressure: 58.60 bar. Thrust to Weight Ratio: 88.64. Country: Russia. First Flight: 1964. Last Flight: 2006. Flown: 1,176. OKB Glushko. Used on Molniya 8K78M and 11A57 Stage 0. Propellants kerosene (RG-1 or T-1) / Lox. Diameter is per chamber.
RD-107-8D728 used on Rocket Stages
Bibliography and Further Reading - Varfolomyev, Timothy, Spaceflight, "Soviet Rocketry that Conquered Space - Part 1", 1995, Volume 37, page 260. 1: Sp 95/37-260; Sp 96/38-31 (8K71 launches); 2: Sp 96/38-48; 3: Sp 96/38-206; Sp 96/38-317 (designatons); 4: Sp 98/40-28; 5:Sp 98/40-85
|
Contact us with any corrections, additions, or comments.
Conditions for use of drawings, pictures, or other materials from this site..
To contact astronauts or cosmonauts.
© Mark Wade, 1997 - 2007 except where otherwise noted.
|
|
|
|