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Summary
| Description |
English: In parallel with a GEO depot a cryogenic depot should be started in LEO. This depot could be used to top-off upper stages with propellant in orbit reducing the launch performance penalty for caring the propellant to space. This capability would have two significant advantages over not using a depot. First it would enable getting more with existing launch vehicles and second it reduce the size of future launch vehicles needed to perform missions with a single launch vehicle). Once this depot capability is operational larger missions can be performed, like going to the Moon, using existing launch vehicles reasonably soon. |
| Date | |
| Source | http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20110013138_2011013651.pdf |
| Author | NASA |
Licensing
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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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| Date/Time | Thumbnail | Dimensions | User | Comment | |
|---|---|---|---|---|---|
| current | 05:39, 31 July 2011 | | 1,094 × 1,067 (102 KB) | Craigboy |
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