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N11 1963
Part of N1
N2
N2
Credit: © Mark Wade
Russian heavy-lift orbital launch vehicle. A military variant of the N-11 which would use a powerful third stage, probably derived from the first stage of the 8K713 GR-1, to put up to 24 metric tons in low earth orbit. This was a competitor with Chelomei's UR-500K, which was selected instead for the heavy military payload mission.

AKA: 11A53. Status: Study 1963. Payload: 24,000 kg (52,000 lb). Thrust: 10,610.00 kN (2,385,220 lbf). Gross mass: 770,000 kg (1,690,000 lb). Height: 60.00 m (196.00 ft). Diameter: 9.80 m (32.10 ft). Apogee: 300 km (180 mi).

LEO Payload: 24,000 kg (52,000 lb) to a 300 km orbit at 51.60 degrees.

Stage Data - N-11 1963



Family: heavy-lift, orbital launch vehicle. Country: Russia. Engines: NK-19, NK-15V. Stages: N-11 1963 - V, N-11 Block A, N-11 Block B. Agency: Korolev bureau.

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