File:RP1357 p17 N-1 rocket configured for lunar flight.svg
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[edit]DescriptionRP1357 p17 N-1 rocket configured for lunar flight.svg |
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). Flight-test version, dubbed T1K, was to have been launched on a Proton rocket. However, the T1K flight-test program was cancelled in favor of all-up testing on the N-1 rocket (figure 1-13).40 Similarly, in 1965, the Apollo program opted for unmanned allup testing. |
Date | |
Source | Mir Hardware Heritage. NASA Reference Publication 1357 (March 1995). |
Author | David S. F. Portree / NASA |
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[edit]Public domainPublic domainfalsefalse |
This file is in the public domain in the United States because it was solely created by NASA. NASA copyright policy states that "NASA material is not protected by copyright unless noted". (See Template:PD-USGov, NASA copyright policy page or JPL Image Use Policy.) | ||
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