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N1 1964
Part of N1
N1-L3 - 1964
N1-L3 - 1964
N1-L3 as per advanced project, 1964
Russian heavy-lift orbital launch vehicle. The N1 launch vehicle for the N1-L3 lunar landing mission as described in the draft project of 1964. Design requirement for the single-launch lunar-orbit-rendezvous lunar landing was 2750 metric tons liftoff mass and 95 metric tons low earth orbit payload. The actual N1 that flew in 1969 to 1972 had lighter first and third stages, but never demonstrated a full fuel load using superchilled propellants as planned in the draft project.

AKA: 11A52;G-1;SL-15. Status: Development ended 1964. Payload: 95,000 kg (209,000 lb). Thrust: 44,000.00 kN (9,891,000 lbf). Gross mass: 2,750,000 kg (6,060,000 lb). Height: 105.00 m (344.00 ft). Diameter: 17.00 m (55.00 ft). Apogee: 225 km (139 mi).

LEO Payload: 95,000 kg (209,000 lb) to a 225 km orbit at 51.60 degrees. Flyaway Unit Cost 1985$: 604.000 million.

Stage Data - N1 1964



Family: heavy-lift, orbital launch vehicle. Country: Russia. Engines: NK-19, NK-15V, NK-15. Stages: N1 1964 - A, N1 1964 - B, N1 1964 - V. Agency: Korolev bureau.

1963 March 21 - . LV Family: N1. Launch Vehicle: N1 1964.
1963 April 28 - . LV Family: N1. Launch Vehicle: N1 1964.
1965 September 1 - . LV Family: N1. Launch Vehicle: N1 1964.
1965 December 31 - . LV Family: N1. Launch Vehicle: N1 1964.

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