File:Mir-15.jpg
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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). |
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| Source | http://ston.jsc.nasa.gov/collections/TRS/_techrep/RP1357.pdf | |||||
| Author | NASA | |||||
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Comment: Is this rocket really related to Mir? --Apoc2400 (talk) 09:28, 5 September 2008 (UTC)
File history
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| Date/Time | Thumbnail | Dimensions | User | Comment | |
|---|---|---|---|---|---|
| current | 04:29, 19 May 2007 | | 363 × 1,632 (116 KB) | Clh288~commonswiki | {{Information |Description=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 |
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