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・ Parkoszewo
・ Parkoszowice, Lesser Poland Voivodeship
・ Parkoszowice, Silesian Voivodeship
・ Parkoszów
・ Parkour
・ Parkour Everyday
・ Parkove
・ Parking lot
・ Parking Lot (song)
・ Parking Lot Party
・ Parking Lots (album)
・ Parking Mad
・ Parking meter
・ Parking Non-Stop
・ Parking on This Side
Parking orbit
・ Parking Panda
・ Parking pawl
・ Parking sensor
・ Parking space
・ Parking Space (film)
・ Parking violation
・ Parking Wars
・ Parkington
・ Parkins Mills, Virginia
・ Parkinson
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・ Parkinson (surname)
・ Parkinson (TV series)
・ Parkinson Association of the Rockies


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Parking orbit : ウィキペディア英語版
Parking orbit
A parking orbit is a temporary orbit used during the launch of a satellite or other space probe. A launch vehicle boosts into the parking orbit, then coasts for a while, then fires again to enter the final desired trajectory. The alternative to a parking orbit is ''direct injection'', where the rocket fires continuously (except during staging) until its fuel is exhausted, ending with the payload on the final trajectory.
==Rationale for parking orbits==
There are several reasons why a parking orbit may be used:
*It can increase the launch window. For earth-escape missions, these are often quite short (seconds to minutes) if no parking orbit is used. With a parking orbit, these can often be increased up to several hours.〔 (Chapter 3.4 )〕
*For non-Low Earth orbit missions, the desired location for the final burn may not be in a convenient spot. In particular, for earth-escape missions that want good northern coverage of the trajectory, the correct place for the final burn is often in the southern hemisphere.
*For geostationary orbit missions, the correct spot for the final (or next to final) firing is normally on the equator. In such a case, the rocket is launched, coasts in a parking orbit until it is over the equator, then fires again into a geostationary transfer orbit.〔, (page 83 ).〕
*For manned lunar missions, a parking orbit allowed some checkout while still close to home, before committing to the lunar trip.〔
*It is needed if the desired orbit has a high perigee. In this case the booster launches into an elliptical parking orbit, then coasts until a higher point in the orbit, then fires again to raise the perigee. See Hohmann transfer orbit. In this case the use of a parking orbit can also reduce the fuel usage of an inclination change, since these take less delta-V at high elevations.
The figure shows the first two reasons. For this lunar mission, the desired location for the final firing is originally over southern Africa. As the day progresses, this point stays essentially fixed while the Earth moves underneath, and this is compensated for by changing the launch angle.

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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