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Navigation and the Mars Global Surveyor Mission

机译:导航和火星全球测量师使命

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The Mars Global Surveyor(MGS) spacecraft was successfully launched from Cape Canaveral by a Delta II 7925 rocket on 11/7/96,17:00:50 UTC.Injection into the trans-Mars trajectory went smoothly with the achieved or reconstructed injection targeting within 1.3 sigma of the planned targeting.As of 6/1/97,we are 205 days into the mission.Two trajectory correction maneuvers(TCM-1 and TCM-2 ) were successfully completed on 11/21/96 and 3/20/97.TCM-3, which was to have occurred on 4/22/97,was cancelled because of the accuracy of previous targeting.The final TCM shall occur on 8/25/97 in order to adjust arrival conditions for the Mars Orbit Insertion(MOI) maneuver which shall occur on 9/12/97.The planned capture orbit is highly elliptical with a 45 hour orbital period,a 300 km periapsis altitude and a descending node at 5:43 pm local mean solar time.
机译:MARS全球测量师(MGS)航天器由Cape Canaveral通过11/7 / 96,17:00:50 UTC.Injection进入Trans-Mars轨迹的普通舞蹈集于Canaveral成功地从Cape Canaveral发射到Trans-Mars轨迹中达到或重建注射靶向在计划目标的1.3中内。6/1 / 97,我们是205天进入Mission.Two轨迹纠正演习(TCM-1和TCM-2)于11/21/96和3/20成功完成/97.TCM-3在4 / 22/97发生,由于先前的目标的准确性取消。最后的中医应在8/25/97发生,以调整火星轨道的到达条件将在9 / 12/97发生的插入(MOI)机动。计划的捕获轨道具有45小时轨道周期,PeriaPsis高度为300 km Periaps Altitude和5:43 PM局部平均太阳时间。

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