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N1F
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Part of N1
N1F - 1974
N1F - 1974
N1F - 1974 Configuration (N1 s/n 8L)
Russian heavy-lift orbital launch vehicle. The N1F would have been the definitive flight version of the N1, incorporating all changes resulting from the four flight tests of the vehicle, including the new Kuznetsov engines and 10% greater liftoff mass by using superchilled propellants in all stages. N1 8L would have been the first N1F configuration flight, with launch planned in the third quarter of 1975 at the time the project was cancelled.

Status: Development ended 1974. Payload: 105,000 kg (231,000 lb). Thrust: 44,400.00 kN (9,981,500 lbf). Gross mass: 3,025,000 kg (6,668,000 lb). Height: 105.00 m (344.00 ft). Diameter: 17.00 m (55.00 ft). Apogee: 220 km (130 mi).

LEO Payload: 105,000 kg (231,000 lb) to a 220 km orbit at 51.60 degrees.

Stage Data - N1F


More at: N1F.

Family: heavy-lift, orbital launch vehicle. Country: Russia. Engines: NK-19, 11D121, NK-39, NK-43, NK-33, RD-58. Spacecraft: L3M-1970, MKBS, L3M-1972. Stages: N1 Block G, N1 Block D, N1F Block A, N1F Block B, N1F Block V. Agency: Korolev bureau.

1970 June - . LV Family: N1. Launch Vehicle: N1F.
1972 February 16 - . LV Family: N1. Launch Vehicle: N1F.
1972 February 23 - . LV Family: N1. Launch Vehicle: N1F.
1972 May 15 - . LV Family: N1. Launch Vehicle: N1F.

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