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N-IUV-III
Part of N1
N-IUV-III
N-IUV-III
Russian heavy-lift orbital launch vehicle. The N-IUV-III would replace the N-IU's conventional third stage with a LOX/LH2 cryogenic third stage. This was seen at the time as the first step in exploitation of cryogenic technology in Russia. Although pursued for some time, this large stage never went into development. The more modestly-sized Block R, Block S, and Block SR instead were put into development in the early 1970's.

Status: Study 1965. Payload: 115,000 kg (253,000 lb). Thrust: 44,000.00 kN (9,891,000 lbf). Gross mass: 2,900,000 kg (6,300,000 lb). Height: 120.00 m (390.00 ft). Diameter: 17.00 m (55.00 ft). Apogee: 220 km (130 mi).

LEO Payload: 115,000 kg (253,000 lb) to a 220 km orbit at 51.60 degrees.

Stage Data - N-IUV-III



Family: heavy-lift, orbital launch vehicle. Country: Russia. Engines: RD-57, NK-15V, NK-15. Stages: N1 Block V-III, N1U 1965 - A, N1U 1965 - B. Agency: Korolev bureau.

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