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N1F 1965 - V
Part of N1 Block V
LOx/Kerosene propellant rocket stage. As per N1 improvement study, 1965. Engine thrust increased and stretched propellant tanks with almost 50% increase.

Status: Study 1965. Thrust: 2,450.00 kN (550,780 lbf). Gross mass: 300,000 kg (660,000 lb). Unfuelled mass: 20,000 kg (44,000 lb). Specific impulse: 347 s. Burn time: 380 s. Height: 16.00 m (52.00 ft). Diameter: 4.80 m (15.70 ft). Span: 6.80 m (22.30 ft).

No Engines: 4.

Country: Russia. Engines: 11D53F. Launch Vehicles: N-IF 1965. Propellants: Lox/Kerosene.
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