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Sub-orbital spaceflight
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Sub-orbital spaceflight : ウィキペディア英語版
Sub-orbital spaceflight

A sub-orbital spaceflight is a spaceflight in which the spacecraft reaches space, but its trajectory intersects the atmosphere or surface of the gravitating body from which it was launched, so that it does not complete one orbital revolution.
For example, the path of an object launched from Earth that reaches above sea level, and then falls back to Earth, is considered a sub-orbital spaceflight. Some sub-orbital flights have been undertaken to test spacecraft and launch vehicles later intended for orbital spaceflight. Other vehicles are specifically designed only for sub-orbital flight; examples include manned vehicles such as the X-15 and SpaceShipOne, and unmanned ones such as ICBMs and sounding rockets.
Flights which attain sufficient velocity to go into low Earth orbit, and then de-orbit before completing their first full orbit, are not considered sub-orbital. Examples of this include Yuri Gagarin's Vostok 1, and flights of the Fractional Orbital Bombardment System.
Usually a rocket is used, but experimental sub-orbital spaceflight has also been achieved with a space gun.
==Altitude requirement==

By one definition a sub-orbital spaceflight reaches an altitude higher than above sea level. This altitude, known as the Kármán line, was chosen by the Fédération Aéronautique Internationale because it is roughly the point where a vehicle flying fast enough to support itself with aerodynamic lift from the Earth's atmosphere would be flying faster than orbital speed.〔
(【引用サイトリンク】title=100 km Altitude Boundary for Astronautics )〕 The US military and NASA award astronaut wings to those flying above ,〔http://www.nasa.gov/centers/dryden/news/NewsReleases/2005/05-57.html〕 although the U.S. State Department appears to not support a distinct boundary between atmospheric flight and spaceflight.〔http://www.state.gov/s/l/22718.htm〕

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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