Vostok 8A92M-1 (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

Vostok 8A92M-1

Part of R-7 Block A stage series

LOx/Kerosene propellant rocket stage. .

Status: Retired 1991. Thrust: 940.40 kN (211,410 lbf). Gross mass: 101,000 kg (222,000 lb). Unfuelled mass: 6,500 kg (14,300 lb). Specific impulse: 315 s. Specific impulse sea level: 248 s. Burn time: 305 s. Height: 28.00 m (91.00 ft). Diameter: 2.99 m (9.80 ft). Span: 2.99 m (9.80 ft).

Cost $ : 13.000 million.

Country: Russia. Engines: RD-108-8D75K. Launch Vehicles: Vostok 8A92M. 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