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Description

English: Figure 1-13. N-1 rocket configured for lunar flight. The basic rocket consisted of the Block A first stage, the Block B second stage, and the Block V third stage. All stages burned liquid oxygen and kerosene. For lunar missions the LRS was added. The N-1 would have delivered about 100,000 kg to low-Earth orbit. (For a comparison with the U.S. Saturn V rocket, see figure 4-1).

Date

March 1995

Source

http://ston.jsc.nasa.gov/collections/TRS/_techrep/RP1357.pdf

Author

NASA

Permission
(Reusing this file)

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Category:PD NASA#Mir-15.jpg

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Comment: Is this rocket really related to Mir? --Apoc2400 (talk) 09:28, 5 September 2008 (UTC)

Category:Media from Mir Hardware Heritage Category:N-1 (rocket)

Wikimore

File:Mir-15.jpg