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-107-8D74PS
Part of RD-107 Family
RD-107
RD-107
Credit: © Mark Wade
Glushko LOx/Kerosene rocket engine. Sputnik 8K71PS-0. Out of Production. OKB Glushko. Used on 8K71PS Stage 0. Developed in 1956-1957. Flown 1957-1958. Propellants kerosene (RG-1) / LOx. Diameter is per chamber.

AKA: 8D74PS. Status: Out of Production. Number: 32 . Thrust: 971.00 kN (218,289 lbf). Unfuelled mass: 1,155 kg (2,546 lb). Specific impulse: 306 s. Specific impulse sea level: 250 s. Burn time: 146 s. Height: 2.86 m (9.38 ft). Diameter: 0.67 m (2.19 ft).

Chambers: 4. Thrust (sl): 793.200 kN (178,318 lbf). Thrust (sl): 80,884 kgf. Engine: 1,155 kg (2,546 lb). Chamber Pressure: 60.00 bar. Area Ratio: 18.9. Thrust to Weight Ratio: 85.71.



Country: Russia. Launch Vehicles: Sputnik 8K71PS. Propellants: Lox/Kerosene. Agency: Glushko bureau.
Photo Gallery

R-7 aft endR-7 aft end
Credit: © 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
© 1997-2017 Mark Wade - Contact
© / Conditions for Use