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
Soyuz 11A511-2
Part of R-7 Block I stage series Family
LOx/Kerosene propellant rocket stage. .

AKA: 11S510. Status: Retired 1975. Thrust: 294.00 kN (66,093 lbf). Gross mass: 25,400 kg (55,900 lb). Unfuelled mass: 2,700 kg (5,900 lb). Specific impulse: 330 s. Burn time: 246 s. Height: 6.74 m (22.11 ft). Diameter: 2.66 m (8.72 ft). Span: 2.66 m (8.72 ft).

Cost $ : 3.000 million.



Country: Russia. Engines: RD-0110. Launch Vehicles: Soyuz 11A511. Propellants: Lox/Kerosene.

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