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skip reentry
Skip reentry is a reentry technique involving one or more successive "skips" off the atmosphere to achieve greater entry range or to slow the spacecraft before final entry, which helps to dissipate the huge amount of heat that is usually generated on faster descents. The range modulation made possible by skip entry allows a spacecraft to reach a wider landing area, or to reach a designated landing point from a wider range of possible entry times, which is especially important in abort situations. Like aerocapture, skip reentry requires precise guidance. An overly shallow entry angle will result in the spacecraft retaining too much of its velocity, possibly escaping into space permanently if this is more than escape velocity. An overly steep entry, on the other hand, results in more intense heating and stress that could exceed the design limits of the spacecraft, potentially destroying it.
== Concept ==
The basic concept is to 'clip' the atmosphere at such an angle that the spacecraft is 'pushed' back out into space, conceptually similar to a flat stone skipping across the surface of a lake. Each time, the spacecraft's velocity is reduced so that it can eventually drop into the atmosphere at a low suborbital velocity.
In theory, any craft could perform skip re-entry as it does not require much lift, but in practice it requires precise guidance. Although the space shuttle was capable of skip reentry, NASA had carried it out only in computer simulations (Scott Horowitz, NASA interview, Jan. 25, 2007). It is unclear how thermal shielding would have fared under the rapid heating, cooling and reheating. In theory STS-107 might have survived if a skip trajectory had been attempted - giving more time for heat dissipation - but this cannot be proven.
Skip entry was first imagined in the 1930s by Eugen Sänger, who proposed a suborbital skipping trajectory for the German Silbervogel bomber, which never flew.
抄文引用元・出典: フリー百科事典『 ウィキペディア（Wikipedia）』
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