N1 Block D

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N1 Block D

Part of Block D

LOx/Kerosene propellant rocket stage. Block D as originally designed as a lunar crasher stage.

Status: Retired 1972. Thrust: 83.30 kN (18,727 lbf). Gross mass: 18,200 kg (40,100 lb). Unfuelled mass: 3,500 kg (7,700 lb). Specific impulse: 349 s. Burn time: 600 s. Height: 5.70 m (18.70 ft). Diameter: 2.90 m (9.50 ft). Span: 2.90 m (9.50 ft).

Family: Space Tugs. Country: Russia. Engines: 11D79, RD-58. Spacecraft: L3. Launch Vehicles: N1, N1F, N1 1969. Propellants: Lox/Kerosene.

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