N-11GR

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

N-11GR - V

Part of Block L

LOx/Kerosene propellant rocket stage. Orbital MIRV stage. Six of these stages clustered around Block B; each stage would have had a 1500 kg nuclear warhead.

Status: Study 1962. Thrust: 88.20 kN (19,828 lbf). Gross mass: 8,200 kg (18,000 lb). Unfuelled mass: 1,700 kg (3,700 lb). Specific impulse: 346 s. Burn time: 246 s. Height: 5.00 m (16.40 ft). Diameter: 2.40 m (7.80 ft). Span: 2.40 m (7.80 ft).

Country: Russia. Engines: 8D726. Launch Vehicles: N111, N11GR. 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