N1 Block G

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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.

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