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21.
The Bastille-day event in 2000 produced energetic 3B/X5.6 flare with a halo CME, which had great geo-effects consequently.
This event has been studied extensively and it is considered that it follows the two-ribbon flare model. The flare/CME event
was triggered by an erupting filament and TRACE observations showed formation of giant arcade structures during the flare
process. Hard X-ray (HXR) two ribbons revealed for the first time in this flare event (Masuda et al., 2001). The reconstruction of 3-D coronal magnetic fields revealed a magnetic flux rope structure, for the first time, from
extrapolation of observed photospheric vector magnetogram data and the flux rope structure was co-spatial with portion of
the filament and a UV bright lane (Yan et al., 2001a, 2001b). Here we review some recent work related to the flux rope structure and the HXR two ribbons by comparing their
locations and the flux temporal profiles during the flare process so as to understand the energy release and particle accelerations.
It is proposed that the rope instability may have triggered the flare event, and reconnection may occur during this process.
The drifting pulsation structure in the decimetric frequency range is considered to manifest the rope ejection, or the initial
phase of the coronal mass ejection. The HXR two ribbons were distributed along the flux rope and the rope foot points coincide
with HXR sources. The energy dissipation from IPS observations occurred within about 100 R
⋅ is consistent with the estimate for the flux rope system.
This revised version was published online in August 2006 with corrections to the Cover Date. 相似文献
22.
一、高度的测量及相关名词含义在空间中,要测量飞机的高度需要两个要素:一是测量基准面,二是从该基准面到飞机的垂直距离。在飞行中,通常采用某个等气压面作为测量基准面,飞机通过机载的气压式高度表测得的气压差来测量垂直距离。不同的等气压面和对应的垂直距离都有特定的名称 相似文献
23.
结合 TMS32 0 C80的编程结构 ,利用神经网络的权并行性和神经元并行性 ,提出了BP算法的并行实现方法 ,并解决了存储器访问冲突、数据双缓冲传输、PP细粒度并行和死锁等问题。结果表明 ,该并行 BP算法十分有效。 相似文献
24.
以50W变换器为例,分别从磁性元件的大小,功率管上的电应力、磁恢复问题,输出纹波及输出特性等方面,详细分析比较了组合式变换器与单端式变换器的优缺点,并给出了具体数据,提出了正-反激组合式变换器具有电压应力低,磁性元件小,体积小,重量轻,输出纹波小及可靠性高的结论。 相似文献
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The Ariane transfer vehicle (ATV), an Ariane 5 borne, unmanned propulsion vehicle, is designed to transport the logistics needed to resupply the International Space Station (ISS) and the man tended free flyer (MTFF) step 2 with pressurized and unpressurized cargo and to dispose the waste. The ATV is an expendable vehicle and is disposed of by a safe atmospheric burn up. In accordance with the AR5 schedule it should be operational in 1996 for missions toward ISS and beyond the year 2000 for MTFF 2 missions. The main constituents of the proposed ATV are the modified AR5 third stage L5, an upgraded VEB steering the launcher as well as the ATV and the P/L-adaptor providing mechanical and umbilical links to the payload. The mechanical part of the RVD-kit will be placed on the payload-module, the main RVD sensors are located on the adaptor and the needed computer intelligence will be integrated on the VEB. To minimize the development, and recurring costs, the ATV concept fully complies to the idea of maximum use of existing hardware and software, mainly from the AR5, Hermes and Columbus programs thus minimizing development and recurring costs. The ATV is compatible to ISS, MTFF and OMV and is able to transport logistic modules compatible with NSTS and U.S.-expendable launchers. 相似文献
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化学气相渗透法制备碳化硅陶瓷复合材料 总被引:1,自引:2,他引:1
综述了化学气相渗透法制备连续纤维增强碳化硅陶瓷复合材料的过程,以及碳化硅陶瓷复合材料的性能及应用。 相似文献
30.