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131.
C. M. Lisse M. F. A’Hearn T. L. Farnham O. Groussin K. J. Meech U. Fink D. G. Schleicher 《Space Science Reviews》2005,117(1-2):161-192
As comet 9P/Tempel 1 approaches the Sun in 2004–2005, a temporary atmosphere, or “coma,” will form, composed of molecules
and dust expelled from the nucleus as its component icy volatiles sublimate. Driven mainly by water ice sublimation at surface
temperatures T > 200 K, this coma is a gravitationally unbound atmosphere in free adiabatic expansion. Near the nucleus (≤ 102 km), it is in collisional equilibrium, at larger distances (≥104 km) it is in free molecular flow. Ultimately the coma components are swept into the comet’s plasma and dust tails or simply
dissipate into interplanetary space. Clues to the nature of the cometary nucleus are contained in the chemistry and physics
of the coma, as well as with its variability with time, orbital position, and heliocentric distance.
The DI instrument payload includes CCD cameras with broadband filters covering the optical spectrum, allowing for sensitive
measurement of dust in the comet’s coma, and a number of narrowband filters for studying the spatial distribution of several
gas species. DI also carries the first near-infrared spectrometer to a comet flyby since the VEGA mission to Halley in 1986.
This spectrograph will allow detection of gas emission lines from the coma in unprecedented detail. Here we discuss the current
state of understanding of the 9P/Tempel 1 coma, our expectations for the measurements DI will obtain, and the predicted hazards
that the coma presents for the spacecraft.
An erratum to this article is available at . 相似文献
132.
Deep Impact Mission Design 总被引:1,自引:0,他引:1
William H. Blume 《Space Science Reviews》2005,117(1-2):23-42
The Deep Impact mission is designed to provide the first opportunity to probe below the surface of a comet nucleus by a high-speed
impact. This requires finding a suitable comet with launch and encounter conditions that allow a meaningful scientific experiment.
The overall design requires the consideration of many factors ranging from environmental characteristics of the comet (nucleus
size, dust levels, etc.), to launch dates fitting within the NASA Discovery program opportunities, to launch vehicle capability
for a large impactor, to the observational conditions for the two approaching spacecraft and for telescopes on Earth. 相似文献
133.
Since its discovery in 1867, periodic comet 9P/Tempel 1 has been observed at 10 returns to perihelion, including all its returns
since 1967. The observations for the seven apparitions beginning in 1967 have been fit with an orbit that includes only radial
and transverse nongravitational accelerations that model the rocket-like thrusting introduced by the outgassing of the cometary
nucleus. The successful nongravitational acceleration model did not assume any change in the comet’s ability to outgas from
one apparition to the next and the outgassing was assumed to reach a maximum at perihelion. The success of this model over
the 1967–2003 interval suggests that the comet’s spin axis is currently stable. Rough calculations suggest that the collision
of the impactor released by the Deep Impact spacecraft will not provide a noticeable perturbation on the comet’s orbit nor
will any new vent that is opened as a result of the impact provide a noticeable change in the comet’s nongravitational acceleration
history. The observing geometries prior to, and during, the impact will allow extensive Earth based observations to complement
the in situ observations from the impactor and flyby spacecraft. 相似文献
134.
王香%于德志%连晓明%李庆芬 《宇航材料工艺》2006,36(4):50-53
采用自蔓延高温合成(SHS)法制备高TiC颗粒含量的TiC/Al复合材料。利用自制的实验装置研究复合材料中TiC颗粒在静止锌液中的均匀化过程。结果表明:当锌液温度低于铝的熔点时,TiC/Al复合材料置于锌液后,锌向其内部扩散,引起复合材料表层内液相线温度降低,当表层内Al-Zn合金的液相线温度等于或低于锌液温度时,Al-Zn合金便处于熔融状态,TiC颗粒随其一起从TiC/Al复合材料块上脱落,并不断地向锌液内部传输,最终均匀分布在锌液中;而当锌液温度高于铝熔点时,TiC/Al复合材料置入后,锌和铝同时进行扩散,但是当复合材料表面温度达到铝熔点时,铝开始熔化,铝的熔化导致TiC颗粒的脱落,脱落下来的TiC颗粒不断向锌液内部传输,最终均匀分布在锌液中。 相似文献
135.
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137.
1/f波动数据的产生及其舒适感分析 总被引:7,自引:0,他引:7
为了获得使人感到舒适的自然风,提出了对风扇转速进行1/f控制的方案,详细论述了1/f波动数据的生成和对风扇电机电压的控制方法,并用单因素方差分析的方法将1/f波动控制产生的舒适感的效果与白噪和1/f 2波动控制方式的情况进行比较,证明了1/f波动控制方式对于提高人的舒适感的有效性. 相似文献
138.
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140.
遥感影像的预处理工作是遥感数据应用的基础。去除云雾是影像预处理工作的重要组成部分。针对遥感影像雾霾浓度分布不均匀的问题,提出一种改进的暗通道遥感影像去雾方法。以"高分一号"(GF-1)卫星为例,根据影像灰度图中的灰度值对影像雾霾浓度区域进行划分,对每个区域中暗原色值的获取方式进行改进,使用导向滤波优化大气传输率,以归一化植被指数(NDVI)为基础,设计用于评价影像去雾质量的定量指标。结果表明:所提出的方法能明显去除雾霾干扰,有效改善卫星影像数据的视觉效果,增强影像细节。该方法去雾处理后的遥感数据能应用于定量遥感,提高遥感影像的可用性及有效性。 相似文献