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The amount of fuel carried on board a satellite directly affects its lifetime, therefore it is desirable to make the apogee kick maneuver as efficient as possible. The mass of most geostationary satellites at the beginning of their operational life in geostationary orbit is typically about half that
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to reach a geostationary orbit. This is typically done with a fixed onboard apogee kick motor. When the satellite reaches its orbit's apogee position, the AKM is ignited, transforming the elliptical orbit into a circular orbit, while at the same time bringing the inclination to around zero degrees,
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A solid-propellant apogee motor for the NATO III communications satellite (SATCOM) is being put into a 110,000-foot altitude test. The engine also underwent the impact, vibration and acceleration (IVA) test.
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More generally, firing a rocket engine to place a vehicle into the desired final orbit from a transfer orbit is labelled an "orbital insertion burn" or, if the desired orbit is circular, a
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when they separated from their vehicle in geostationary transfer orbit, with the other half having been fuel expended in the apogee kick maneuver.
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thereby accomplishing the insertion into a geostationary orbit. This process is called an "apogee kick".
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Kick In the Apogee: 40 years of upper stage applications for solid rocket motors, 1957–1997
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329:. The Johns Hopkins University Applied Physics Laboratory. 18 November 2005.
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An apogee kick motor is used, for example, for satellites launched into a
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For orbits around bodies other than Earth, it may be referred to as an
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to provide the final impulse to change the trajectory from the
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of the launch site. This orbit is commonly known as a "
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327:"New Horizons Launch Preparations Move Ahead"
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160:at a significant distance away from Earth's
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80:Learn how and when to remove this message
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301:. John Wiley & Sons Inc. pp.
111:Arnold Engineering Development Complex
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141:into its final orbit (most commonly
49:it lacks sufficient corresponding
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297:The Complete Book of Spaceflight
221:Advanced Cryogenic Evolved Stage
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196:Use on interplanetary missions
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170:geostationary transfer orbit
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211:spacecraft towards Pluto.
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62:introducing
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293:(2003).
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