RD-107-8D728 (original) (raw)

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-107-8D728

Part of RD-107

RD-107
Credit: © Mark Wade

Glushko LOx/Kerosene rocket engine. Molniya 0, Molniya 8K78M-0. OKB Glushko. Used on Molniya 8K78M and 11A57 Stage 0. Propellants kerosene (RG-1 or T-1) / LOx. Diameter is per chamber. First flight 1964.

AKA: 8D728. Number: 1176 . Thrust: 996.00 kN (223,909 lbf). Unfuelled mass: 1,145 kg (2,524 lb). Specific impulse: 314 s. Specific impulse sea level: 257 s. Burn time: 120 s. Height: 2.86 m (9.38 ft). Diameter: 0.67 m (2.19 ft).

Chambers: 4. Thrust (sl): 818.800 kN (184,074 lbf). Thrust (sl): 83,484 kgf. Engine: 1,145 kg (2,524 lb). Chamber Pressure: 58.60 bar. Thrust to Weight Ratio: 88.64.

Country: Russia. Launch Vehicles: Molniya 8K78M. Propellants: Lox/Kerosene. Stages: Molniya 8K78M-0. Agency: Glushko bureau.

Photo Gallery

	R-7 aft endCredit: © Mark Wade

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