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A Liquid Apogee Engine (LAE), or apogee engine, refers to a type of chemical rocket engine typically used as the main engine in a spacecraft. The name ''apogee engine'' derives from the type of manoeuvre for which the engine is typically used i.e. an in-space delta-''v'' change made at the apogee of an elliptical orbit in order to circularise it. For geostationary satellites, this type of orbital manoeuvre is performed to transition from a geostationary transfer orbit and place the satellite on station in a circular geostationary orbit. Despite the name, an apogee engine can be used for a range of other manoeuvres such as end-of-life deorbit,〔 earth orbit escape, planetary orbit insertion and planetary decent/ascent.〔(【引用サイトリンク】url=http://emits.sso.esa.int/emits-doc/ESTEC/ESAIPC(2010)136_RobotExp2009-2014.pdf )〕 In some parts of the space industry an LAE is also referred to as a Liquid Apogee Motor (LAM), a Liquid Apogee Thruster (LAT) and, depending on the propellant, a Dual Mode Liquid Apogee Thruster (DMLAT). Despite the ambiguity with respect to the use of ''engine'' and ''motor'' in these names, all use liquid propellant. An Apogee Kick Motor (AKM) or Apogee Boost Motor (ABM) such as the Waxwing however uses solid propellant. These solid propellant versions are not used on new generation satellites.〔 ==History== The apogee engine traces its origin to the early 1960s when companies such as Aerojet, Rocketdyne, Reaction Motors, Bell Aerosystems, TRW Inc. and The Marquardt Company were all participants in developing engines for various satellites and spacecraft. Derivatives of these original engines are still used today and are continually being evolved〔(【引用サイトリンク】url=http://www.layerwise.com/esa-investigates-alm-for-satellite-engines/ )〕 and adapted for new applications. 抄文引用元・出典: フリー百科事典『 ウィキペディア（Wikipedia）』 ■ウィキペディアで「Liquid Apogee Engine」の詳細全文を読む スポンサード リンク
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