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N-IF 1965
Part of N1
N-IF Variants
N-IF Variants
N-IF Versions, from left: N1-L3; N-IF; N-IUV-III; N-IFV-III; N-IFV-III,II
Russian heavy-lift orbital launch vehicle. The N-IF would be the first follow-on version with increased performance. The first stage engines would be increased in thrust from an average of 150 metric tons to 175 metric tons, and those in the second stage from 150 metric tons to 200 metric tons. The second and third stages would be substantially enlarged.

Status: Study 1965. Payload: 100,000 kg (220,000 lb). Thrust: 51,500.00 kN (11,577,600 lbf). Gross mass: 2,950,000 kg (6,500,000 lb). Height: 110.00 m (360.00 ft). Diameter: 17.00 m (55.00 ft). Apogee: 220 km (130 mi).

LEO Payload: 100,000 kg (220,000 lb) to a 220 km orbit at 51.60 degrees.

Stage Data - N-IF 1965



Family: heavy-lift, orbital launch vehicle. Country: Russia. Engines: 11D51F, 11D52F, 11D53F. Stages: N1F 1965 - A, N1F 1965 - B, N1F 1965 - V. Agency: Korolev bureau.

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