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
N1 Block G
LOx/Kerosene propellant rocket stage. Empty mass estimated.

Status: Retired 1972. Thrust: 446.00 kN (100,264 lbf). Gross mass: 61,800 kg (136,200 lb). Unfuelled mass: 6,000 kg (13,200 lb). Specific impulse: 353 s. Burn time: 443 s. Height: 9.10 m (29.80 ft). Diameter: 4.40 m (14.40 ft). Span: 4.40 m (14.40 ft).



Subtopics

N-11 1963 - V LOx/Kerosene propellant rocket stage. Conjectural stage derived from GR-1 stage 1 to match total mass given of launch vehicle.

GR-1 Stage 1 LOx/Kerosene propellant rocket stage. Payload 4,000 kg (2.2 MT nuclear warhead). Range 13,000 km or orbital. Accuracy (90%) 5 km in range and 3 km in dispersion. Masses estimated based on total vehicle mass of 117 metric tons.

Country: Russia. Engines: NK-19. Launch Vehicles: N1, N1F, N1 1969. 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