对银行信贷风险形成因素的分析

银行信贷风险是重要的金融风险，笔者对银行信贷风险形成机理和因素作了较详细地分析。     

军用飞机推行综合保障工程的研究

阐述了ILS的涵义及ILS在军用飞机形成战斗力中的重要作用,结合军用飞机实施ILS的现状,对大力推行军用飞机ILS的实施提出了几点建议。     

河南省金融产业竞争力评价与对策

以河南省为研究重点，选取了31个省份作为对照样本，这用主成分和因子分析法对各个区域的金融产业竞争力进行计量分析和排序，结果认为，东部地区金融产业竞争力仍然保持着绝对优势地位，中部六省中，河南省的金融产业竞争力发挥着龙头作用，被划入我国区域金融产业发展的前三个梯度内，表现出良好的发展态势。在对金融产业竞争力的模糊曲线分析后认为，影响金融产业竞争力提高的八个分力，依其重要程度依次为经济力、科技力、文化力、开放力、设施力、劳动力、聚集力和环境力，均对其产生正向贡献。因此，提高河南省金融产业竞争力，主要应从以下方面入手：（1）促进河南省经济的继续增长，努力提高人均可支配收入水平。（2）做好对内对外开放，尤其是针对不同区域有针对性地扩大对外开放与区际开放。（3）完善对外金融交往基础设施，加强政府的监管效率。（4）拓展河南金融业的发展空间，充分发挥其就业效应。（5）进一步加大科技成果的转化。（6）加强区域向心吸引力，促进产业集聚。（7）加强文化建设，完善金融生态环境。     

EVA与现金流量在企业财务战略中的影响及应用

财务战略是企业战略的隶属部分 ,在企业战略中居于核心地位。EVA及现金流量与资本联系紧密 ,反映了企业创造的价值和资金的运转状况 ,两者已经成为衡量企业绩效的最重要指标。结合EVA和现金流量在财务管理中的作用 ,运用财务状况四分图区分企业所处的财务状况 ,为处于不同财务状况的企业提供相匹配的财务战略。     

国际审计准则综论

本文就国际审计准则的产生与发展、制定主体、目的与性质,对各国的影响及利用情况等方面作了概括论述,以求为研究国际审计准则的进程与发展趋势,及对我国制定审计准则提供有益经验。     

Assessment of the consequences of the Fengyun-1C breakup in low Earth orbit

On 11 January 2007, the People’s Republic of China conducted a successful anti-satellite test against one of their defunct polar-orbiting weather satellites. The target satellite, called Fengyun-1C, had a mass of 880 kg and was orbiting at an altitude of about 863 km when the collision occurred. Struck by a direct-ascent interceptor at a speed of 9.36 km/s, the satellite disintegrated, spreading the cataloged fragments between 200 and 4000 km, with the highest concentration near the breakup height. By the end of April 2008, 2377 pieces of debris, including the original payload remnant, had officially been cataloged by the US Space Surveillance Network. Of these, nearly 1% had reentered the Earth’s atmosphere. This deliberate act is the largest debris-generating event on record, and its consequences will adversely affect circumterrestrial space for many years.     

论民航运输企业管理以财务管理为中心

分析了民航运输企业管理的现状,提出并论述了民航运输企业管理以财务管理为中心的依据,阐述了民航运输企业管理以财务管理为中心的特征与标志,说明了今后在财务管理方面应作的工作。     

民航机场风险评价模型应用探讨

机场安全是民航安全管理的重点之一,是正确的指导民航风险管理工作的重要内容.在对民航机场进行风险因素辨识及风险分析的基础上,利用层次分析法和模糊数学理论建立了民航机场风险评价模型,并以首都机场为评价对象,对其进行了风险评价.     

Cellular communication and “non-targeted effects”: Modelling approaches

During the last decade, a large number of experimental studies on the so-called “non-targeted effects”, in particular bystander effects, outlined that cellular communication plays a significant role in the pathways leading to radiobiological damage. Although it is known that two main types of cellular communication (i.e. via gap junctions and/or molecular messengers diffusing in the extra-cellular environment, such as cytokines, NO etc.) play a major role, it is of utmost importance to better understand the underlying mechanisms, and how such mechanisms can be modulated by ionizing radiation. Though the “final” goal is of course to elucidate the in vivo scenario, in the meanwhile also in vitro studies can provide useful insights. In the present paper we will discuss key issues on the mechanisms underlying non-targeted effects and cell communication, for which theoretical models and simulation codes can be of great help. In this framework, we will present in detail three literature models, as well as an approach under development at the University of Pavia. More specifically, we will first focus on a version of the “State-Vector Model” including bystander-induced apoptosis of initiated cells, which was successfully fitted to in vitro data on neoplastic transformation supporting the hypothesis of a protective bystander effect mediated by apoptosis. The second analyzed model, focusing on the kinetics of bystander effects in 3D tissues, was successfully fitted to data on bystander damage in an artificial 3D skin system, indicating a signal range of the order of 0.7–1 mm. A third model for bystander effect, taking into account of spatial location, cell killing and repopulation, showed dose–response curves increasing approximately linearly at low dose rates but quickly flattening out for higher dose rates, also predicting an effect augmentation following dose fractionation. Concerning the Pavia approach, which can model the release, diffusion and depletion/degradation of candidate signals (e.g. cytokines) travelling in the extra-cellular environment, the good agreement with ad hoc experimental data obtained in our laboratory validated the adopted approach, which in the future can be applied also to other candidate signals.     

Micro-meteoroids and space debris impact risk assessment for the ConeXpress satellite using ESABASE2/Debris

Micro-meteoroid and space debris impact risk assessments are performed to investigate the risk from hypervelocity impacts to sensitive spacecraft sub-systems. For these analyses, ESA’s impact risk assessment tool ESABASE2/Debris is used. This software tool combines micro-particle environment models, damage equations for different shielding designs and satellite geometry models to perform a detailed 3D micro-particle impact risk assessment. This paper concentrates on the impact risk for exposed pressurized tanks. Pressure vessels are especially susceptible to hypervelocity impacts when no protection is available from the satellite itself. Even small particles in the mm size range can lead to a fatal burst or rupture of a tank when impacting with a typical collision velocity of 10–20 km/s. For any space mission it has to be assured that the impact risk is properly considered and kept within acceptable limits. The ConeXpress satellite mission is analysed as example. ConeXpress is a planned service spacecraft, intended to extend the lifetime of telecommunication spacecraft in the geostationary orbit. The unprotected tanks of ConeXpress are identified as having a high failure risk from hypervelocity impacts, mainly caused by micro-meteoroids. Options are studied to enhance the impact protection. It is demonstrated that even a thin additional protective layer spaced several cm from the tank would act as part of a double wall (Whipple) shield and greatly reduce the impact risk. In case of ConeXpress with 12 years mission duration the risk of impact related failure of a tank can be reduced from almost 39% for an unprotected tank facing in flight direction to below 0.1% for a tank protected by a properly designed Whipple shield.