Ion relaxation processes in the heliospheric interface: how perturbed are ion distribution functions?

Charge-exchange processes between interstellar H-/O-atoms and protons of the bulk of the interstellar plasma flow downstream of the outer bowshock in the heliospheric interface induce secondary ions leading to non-relaxated velocity distribution functions. The relaxation of these freshly induced ions towards an equilibrium distribution occurs due to Coulomb interactions and wave–particle interactions with the background turbulence. Since Coulomb interactions are of low relevance, we study here in detail the effect of wave–particle interactions. To find the turbulence levels in the interface we consider the MHD-wave transformation at the outer shock surface between the interface and the local interstellar plasma. The turbulence in the outer interface region is shown to be dominated by incompressible Alfvén waves both for cases of quasiparallel and quasiperpendicular shocks. Also we show that waves propagating towards the shock are more intensive than those propagating away from it. The level of Alfvén turbulence in the interface is estimated using the recent data on local interstellar turbulence deduced from observations of interstellar scintillations of distant radiosources. Two proton relaxation processes are considered: quasilinear resonant interactions with Alfvén waves and non-linear self-induced wave–particle scattering. The corresponding diffusion coefficients are estimated, and typical time periods for protons and oxygen ions relaxation are shown to be of the same order of magnitude as H-/O-atoms passage time over the extent of the interface. This indicates that perturbed ion distribution functions must be expected there.     

Coupling of the interstellar and interplanetary magnetic fields at the heliospheric interface: The effect of neutral hydrogen atoms

We present numerical results showing the effect of neutral hydrogen atoms on the solar wind (SW) interaction with the local interstellar medium (LISM), where the interstellar magnetic field (ISMF) is coupled to the interplanetary magnetic field (IMF) at the surface of the heliopause. The IMF on the inner boundary surrounding the Sun is specified in the form of a Parker spiral and self-consistently develops in accordance with the SW motion inside the heliopause. The model of the SW–LISM interaction involves both plasma and neutral components which are treated as fluids. The configuration is chosen where the ISMF is orthogonal to the LISM velocity and tilted 60° to the ecliptic plane. This orientation of the magnetic field is a possible explanation of the 2–3 kHz emission data which is believed to originate ahead of the heliopause. It is shown that the topology of the heliospheric current sheet is substantially affected by the ISMF. The interaction pattern dependence on the neutral hydrogen density is analyzed.     

空间尘埃的充电过程及与等离子体参数的关系

考虑了地球附近的彗星、行星环、行星际介质等空间尘埃等离子体环境中尘埃颗粒的充电问题．应用典型的空间尘埃等离子体参数，计算了不同种类的尘埃颗粒，以及不同等离子体成分下等离子体中尘粒的平衡电势，得到了尘埃颗粒的平衡电势与尘埃等离子体成分、温度，及其他等离子体参数之间的相互关系．     

我国中小企业发展中存在的问题与对策

近几年我国中小企业发展比较迅速，但是中小企业目前所面临的困难也很多。要改变中小企业的生存环境和促进中小企业快速发展，除了企业加强自身能力外，社会尤其是政府应当在政策上给予扶持，在各方面给予中小企业提供帮助，使中小企业快速、健康地发展。     

T cell regulation in microgravity – The current knowledge from in vitro experiments conducted in space,parabolic flights and ground-based facilities

Dating back to the Apollo and Skylab missions, it has been reported that astronauts suffered from bacterial and viral infections during space flight or after returning to Earth. Blood analyses revealed strongly reduced capability of human lymphocytes to become active upon mitogenic stimulation. Since then, a large number of in vitro studies on human immune cells have been conducted in space, in parabolic flights, and in ground-based facilities. It became obvious that microgravity affects cell morphology and important cellular functions. Observed changes include cell proliferation, the cytoskeleton, signal transduction and gene expression. This review gives an overview of the current knowledge of T cell regulation under altered gravity conditions obtained by in vitro studies with special emphasis on the cell culture conditions used. We propose that future in vitro experiments should follow rigorous standardized cell culture conditions, which allows better comparison of the results obtained in different flight- and ground-based experiment platforms.     

Analysis of front plate＇s effect on low hysteresis brush seal

针对不同前板结构的低滞后刷式密封,采用多孔介质模型,进行流场计算,对计算得到的上游刷丝压力、速度分布、刷丝上游靠近跑道区域的湍流动能以及刷式密封泄漏量进行分析,讨论对于低滞后刷式密封的性能的影响．分析表明：前板结构对上游刷丝压力、轴向速度分布以及刷式密封泄漏量无明显影响,对上游刷丝径向速度分布影响较大;无前板及过长前板结构,刷封上游靠近跑道区域湍流动能较大,前板开孔可降低刷丝上游靠近跑道区域的湍流动能,减弱刷丝扰动的趋势．     

小型平板CPL实现高热流密度散热的研究

针对小型平板毛细抽吸两相流体回路(CPL)在高热流密度下的特点,分析了不同工质时系统的压力损失与毛细芯的毛细抽吸力,得出采用氨工质有着较好的传热性能和更高的毛细限,同时得出影响系统毛细限的主要因素是蒸汽联管管径和工质的蒸气密度,提出了工质传输系数作为选取工质的重要指标。建立了蒸发器多孔芯,金属壁面以及工质气、液空间区域的耦合数学模型,并运用SIMPLE算法进行求解,得出蒸发器内的温度分布及由于侧壁效应对多孔芯传热传质与传热极限的影响,同时提出小型平板CPL系统存在侧壁效应传热极限,它是影响系统最大传热量的一个重要极限,在设计小型平板CPL必须予以考虑。     

GHRS observations of the LISM

The GHRS has obtained high-resolution spectra of interstellar gas toward 19 nearby stars. These excellent data show that the Sun is located inside the Local Interstellar Cloud (LIC) with other warm clouds nearby. I will summarize the physical properties of these clouds and the three-dimensional structure of this warm interstellar gas. There is now clear evidence that the Sun and other late-type stars are surrounded by hydrogen walls in the upwind direction. The D/H ratio probably has a constant value in the LIC, (1.6 ± 0.2) × 10^–5, consistent with the measured values for all LIC lines of sight.     

铋工质阳极层推力器的研究与发展

阳极层推力器(TAL)作为一种高功率、比冲、效率的电推力器逐渐成为国内外研究机构关注的重点，其在深空探测领域具有巨大应用潜力。然而，传统的氙工质不仅价格昂贵、提纯难度大、需要高压贮存，而且不能充分发挥TAL的性能优势。固体金属铋工质具有贮存密度高、成本低、易电离等特点成为代替氙工质的理想选择。本文根据TAL的工作原理与结构特点，对铋工质的适用性进行论述。首先对该推力器的研究现状和发展趋势进行概述;其次对铋工质的性能优势进行了阐述;然后对该推力器的结构组成、工作原理及关键技术进行总结与分析;最后对该推力器的应用前景进行展望。     

航空数据存储卡毁钥能力评价方法研究

为满足复杂战场态势下机载数据的安全性需求，需要建立对航空数据存储卡毁钥能力有效评价的方法。 建立航空数据存储卡毁钥能力有效性评价的目的是保证航空装备信息安全的重要措施，是科学、准确评价毁钥 设计是否满足需求的重要手段，是航空装备定型列装前必要的信息安全测评过程。通过对航空数据存储卡的典 型结构和硬件毁钥原理进行分析，对毁钥后电学、物理和化学等技术手段进行深入的研究，提出一种针对航空 数据存储卡毁钥能力的评价方法，从数据存储卡读取能力和存储介质损毁状态两个过程对毁钥效果开展评价， 从而规范了当前测评机构对数据存储卡毁钥能力评价过程中无统一方法的现状。本文利用该评价方法对某样品 航空数据存储卡经硬件毁钥试验后开展毁钥效果分析，验证方法的有效性。航空数据存储卡毁钥能力评价方法 可以很好的评估毁钥设计的效果，确保机载数据的安全。