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Trans Lunar Injection

From Biocrawler, the free encyclopedia.

Trans Lunar Injection (TLI) is a term describing the propulsion maneuver used to set a spacecraft on a trajectory which will intersect the Moon.

The spacecraft is usually in a parking orbit around Earth at the time of TLI.

The maneuver is usually performed by a rather large rocket engine. On the Apollo missions it was performed by the restartable third (S-IVB) stage of the Saturn V rocket. This particular TLI burn lasted approximately 346 seconds, providing 10,000 to 10,600 ft/s (3 to 5 km/s) of delta-v, at which point the spacecraft was travelling at approximately 24,500 mph (39,420 km/h).

Wikipedia (http://en.wikipedia.org/wiki/Main_Page) Trans_Lunar_Injection (http://en.wikipedia.org/wiki/Trans_Lunar_Injection) version history (http://en.wikipedia.org/w/index.php?title=Trans_Lunar_Injection&action=history) GNU Free Documentation Lizenz (http://en.wikipedia.org/wiki/Wikipedia:Text_of_the_GNU_Free_Documentation_License) CC-by-sa (http://creativecommons.org/licenses/by-sa/2.5/)

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