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Trajectory Design and Orbit Determination for the Lunar CRater Observation and Sensing Satellite (LCROSS)

机译:月球喷枪观察和传感卫星(LCross)的轨迹设计和轨道测定

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The Lunar CRater Observation and Sensing Satellite (LCROSS) was competitively selected by the National Aeronautical and Space Administration (NASA) Exploration Systems Mission Directorate (ESMD) as a low-cost (<$80M) 1000 kg secondary payload to be launched with the Lunar Reconnaissance Orbiter (LRO) in October of 2008. LCROSS is a lunar impactor mission that will investigate the presence or absence of water in a permanently shadowed crater. Following launch, trans-lunar injection (TLI) and separation from LRO, LCROSS will remain attached to the launch vehicle's ~2300 kg spent Earth Departure Upper Stage (EDUS) and will guide it toward an impact of a permanently shadowed crater at the lunar South Pole. Hours prior to impact, LCROSS will separate from the EDUS and perform a braking maneuver that will allow the spacecraft to take measurements of the resulting EDUS impact ejecta cloud for several minutes, before impacting the crater as well.
机译:农历火山口观察和传感卫星(LCROSS)被国家航空航天和空间管理(NASA)勘探系统使命(ESMD)作为低成本(<80米)1000公斤的二级有效载荷,以与月球发射 2008年10月的侦察轨道 推出后,Trans-Lunar注射(TLI)和LRO的分离,LCROSS将保持连接到发射车辆的〜2300公斤的地球出发的上阶段(EDU),并将引导它对一个永久阴影火山口在农历南部的影响 极。 撞击前的数小时,LCROSS将与EDU分开,并执行制动机动,使得航天器在撞击火山口之前将导致的EDUS撞击喷射物云进行测量。

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