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On the fast zonal transport of the STS-121 space shuttle exhaust plume in the lower thermosphere

机译:关于STS-121航天飞机尾气羽在低热层的快速区域运输

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Meier et al. (2011) reported rapid eastward transport of the STS-121 space shuttle (launch: July 4, 2006) main engine plume in the lower thermosphere, observed in hydrogen Lyman α images by the GUVI instrument onboard the TIMED satellite. In order to study the mechanism of the rapid zonal transport, diagnostic tracer calculations are performed using winds from the Thermosphere Ionosphere Mesosphere Electrodynamics General Circulation Model (TIME-GCM) simulation of July, 2006. It is found that the strong eastward jet at heights of 100-110. km, where the exhaust plume was deposited, results in a persistent eastward tracer motion with an average velocity of 45. m/s. This is generally consistent with, though faster than, the prevailing eastward shuttle plume movement with daily mean velocity of 30. m/s deduced from the STS-121 GUVI observation. The quasi-two-day wave (QTDW) was not included in the numerical simulation because it was found not to be large. Its absence, however, might be partially responsible for insufficient meridional transport to move the tracers away from the fast jet in the simulation. The current study and our model results from Yue and Liu (2010) explain two very different shuttle plume transport scenarios (STS-121 and STS-107 (launch: January 16, 2003), respectively): we conclude that lower thermospheric dynamics is sufficient to account for both very fast zonal motion (zonal jet in the case of STS-121) and very fast meridional motion to polar regions (large QTDW in the case of STS-107).
机译:Meier等。 (2011年)报道了STS-121航天飞机(于2006年7月4日发射)在较低热圈的主要引擎羽流快速向东运输,这是由TIMED卫星上的GUVI仪器在氢Lymanα图像中观察到的。为了研究快速区域传输的机理,利用2006年7月的热球电离层中层电动力学通用环流模型(TIME-GCM)模拟的风进行了诊断示踪剂计算。发现高空向东射流强度为。 100-110。排气羽沉积的公里数,导致示踪剂持续向东运动,平均速度为45. m / s。这通常与从STS-121 GUVI观测得出的,以日平均速度为30. m / s的普遍的向东穿梭羽流运动(尽管要快)相一致。准两日波(QTDW)未包含在数值模拟中,因为发现它不大。但是,它的缺失可能部分导致子午线传输不足,无法在仿真中将示踪剂从快速射流上移开。当前的研究以及来自Yue和Liu(2010)的模型结果解释了两种截然不同的航天飞机羽流运输情景(分别为STS-121和STS-107(发射时间:2003年1月16日)):我们得出结论,较低的热圈动力学就足够了考虑到非常快速的纬向运动(在STS-121情况下为纬向射流)和到极地区域的非常快的子午运动(在STS-107情况下为大QTDW)。

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