N-IFV-II-III
Launch vehicle · Russia
Original archive entry. The text, images and links below are kept as they were written.
N-IFV-II, III of 1965
Russian heavy-lift orbital launch vehicle. N-IFV-II, III would use only the first stage from the N-1F, and use new cryogenic second and third stages. This cryogenic second stage seems not to have been pursued beyond the study phase.
LEO Payload: 150,000 kg (330,000 lb) to a 220 km orbit at 51.60 degrees.
Related
- Family
- heavy-lift, orbital launch vehicle
- Country
- Russia
- Stages
- N1 Block V-II, N1 Block V-III, N1F 1965 - A
- Agency
- Korolev bureau