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N-IMV-III
Part of N1
N-IMV-III
N-IMV-III
Russian heavy-lift orbital launch vehicle. Then N-IMV-III would add the Block V-III cryogenic third stage to the first and second stages of the N-IM. This provided the second-highest performance of the variations considered and would certainly have been cheaper than the N-IFV-II, III.

Status: Study 1965. Payload: 185,000 kg (407,000 lb). Thrust: 74,000.00 kN (16,635,000 lbf). Gross mass: 4,950,000 kg (10,910,000 lb). Height: 145.00 m (475.00 ft). Diameter: 17.00 m (55.00 ft). Apogee: 220 km (130 mi).

LEO Payload: 185,000 kg (407,000 lb) to a 220 km orbit at 51.60 degrees.

Stage Data - N-IMV-III



Family: heavy-lift, orbital launch vehicle. Country: Russia. Engines: RD-57, 11D51M, 11D52M. Stages: N1 Block V-III, N1M 1965 - A, N1M 1965 - B. Agency: Korolev bureau.

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