N1FV-III - N-IFV-III design of 1965 4,834 bytes. 73 x 401 pixels.

Then N-IFV-III would add the Block V-III cryogenic third stage to the first and second stages of the N-IF.

LEO Payload: 125,000 kg. to: 220 km Orbit. at: 51.6 degrees. Liftoff Thrust: 5,250,000 kgf. Total Mass: 3,000,000 kg. Core Diameter: 17.0 m. Total Length: 125.0 m.

• Stage Number: 1. 1 x N1F 1965 - A Gross Mass: 1,940,000 kg. Empty Mass: 200,000 kg. Thrust (vac): 5,870,000 kgf. Isp: 331 sec. Burn time: 100 sec. Isp(sl): 296 sec. Diameter: 10.0 m. Span: 17.0 m. Length: 30.0 m. Propellants: Lox/Kerosene No Engines: 30. 11D51F

• Stage Number: 2. 1 x N1F 1965 - B Gross Mass: 590,000 kg. Empty Mass: 60,000 kg. Thrust (vac): 1,600,000 kgf. Isp: 346 sec. Burn time: 115 sec. Diameter: 6.8 m. Span: 9.8 m. Length: 26.0 m. Propellants: Lox/Kerosene No Engines: 8. 11D52F

• Stage Number: 3. 1 x N1 Block V-III Gross Mass: 325,000 kg. Empty Mass: 35,000 kg. Thrust (vac): 240,000 kgf. Isp: 440 sec. Burn time: 510 sec. Diameter: 8.0 m. Span: 8.0 m. Length: 27.0 m. Propellants: Lox/LH2 No Engines: 6. RD-57

• 283 - Vetrov, G S, S. P. Korolev i evo delo, Nauka, Moscow, 1998.