A new global F2 peak electron density model for the International Reference Ionosphere (IRI)

A new neural network (NN) based global empirical model for the F2 peak electron density (NmF2) has been developed using extended temporal and spatial geophysical relevant inputs. Measured ground based ionosonde data, from 84 global stations, spanning the period 1995 to 2005 and, for a few stations from 1976 to 1986, obtained from various resources of the World Data Centre (WDC) archives (Space Physics Interactive Data Resource SPIDR, the Digital Ionogram Database, DIDBase, and IPS Radio and Space Services) have been used for training a NN. The training data set includes all periods of quiet and disturbed magnetic activity. A comprehensive comparison for all conditions (e.g., magnetic storms, levels of solar activity, season, different regions of latitudes, etc.) between foF2 value predictions using the NN based model and International Reference Ionosphere (IRI) model (including both the International Union of Radio Science (URSI) and International Radio Consultative Committee (CCIR) coefficients) with observed values was investigated. The root-mean-square (RMS) error differences for a few selected stations are presented in this paper. The results of the foF2 NN model presented in this work successfully demonstrate that this new model can be used as a replacement option for the URSI and CCIR maps within the IRI model for the purpose of F2 peak electron density predictions.     

一种适合P2PMMOG的安全同步算法

为了保证游戏通信协议具有较好的状态同步和防欺骗能力,提出一种适合P2P MMOG的安全同步算法.该算法在防欺骗协议NEO中加入事件排序和基于事件关联的回滚机制,在保证更新信息安全交换的基础上,对游戏事件进行排序,并对迟到事件进行处理.实验结果表明,该算法保证了较好的回滚次数和响应时间,可以有效维护游戏状态的一致性.在防欺骗和游戏状态同步的基础上维护了游戏的公平性.     

A European probe to comet Halley

A European probe to comet Halley is proposed. The probe's model payload consists of 8 scientific instruments, viz. neutral, ion and dust impact mass spectrometers, magnetometer, medium energy ion and electron analyzer, camera, dust impact detectors and plasma wave experiment. Fly-by of the comet Halley nucleus will take place on November 28th, 1985, at about 500 km miss distance. The main spacecraft serves as relay link to transmit the observed data to Earth. As probe, a modified ISEE 2 design is proposed. Because of the cometary dust hazard expected in the coma a heavy dust shield (27 kg) is required, consisting of a thin front sheet and a 3 layer rear sheet. The probe is spin-stabilized (12 rpm), has no active attitude and orbit control capability and uses battery power only to provide about 1000 Wh for a measuring phase. A despun antenna transmits up to 20 kbit/s, in X-band. The total probe mass is estimated at 250 kg. The 3 model development programme should start in mid 1981 with Phase B.     

正电子素的络合作用

本文介绍了正电子素及其络合作用。讨论了正电子素络合反应速度常数的测量方法。比较了几种线性自由能的表达式。     

SiO2 气凝胶热参数测试及评价

利用非稳态阶跃平面热源法对SiO2气凝胶的热参数进行了高温实验研究,获得了不同温度和压力条件下SiO2气凝胶的热导率、热扩散率以及比热容等.结果表明,SiO2气凝胶800℃的热导率比室温增大约62％.在相同气压且低于600℃时,其热导率受比热容影响,而在高于600℃时,则受热扩散率影响;在相同温度且高于10 kPa时,热导率亦受热扩散率影响.     

阳离子对零价铁修复铬污染水体的影响

为了研究阳离子存在对零价铁去除水体中铬污染的影响,在实验室条件下,通过批次实验考察了零价铁在Ca2+、Mg2+单独存在及共存时去除水体中铬污染的效果。结果表明:Ca2+,Mg2+单独存在及共存时,零价铁都可以有效去除水体中的铬污染。前者促进作用不明显,后者促进作用较大。二者共存也可以促进零价铁去除水体中铬污染,且促进作用高于二者单独存在体系。     

动量矩方程的剪切积分解析表示式

本文采用两层涡粘性模型和速度剖面的指数律,导出了可压缩动量矩方程的剪切积分解析表示式,从而大大简化了边界层计算。和其它理论结果相比,本结果更接近于实验数据。     

富铈稀土对氧化锆泡沫陶瓷过滤器性能及晶相组织结构的影响

通过实验，研究了富铈稀土对氧化锆泡沫陶瓷机械性能及晶相组织结构的影响，探索了以MgO稳定氧化锆为基体材料，通过加入适量的富铈稀土来提高氧化锆泡沫陶瓷过滤器韧性和抗压强度的可能性。     

Future X-ray astronomy missions of Japan

Japanese future space programs for high energy astrophysics are presented. The Astro-E2 mission which is the recovery mission of the lost Astro-E has been approved and now scheduled to be put in orbit in early 2005. The design of the whole spacecraft remains the same as that of Astro-E, except for some improvements in the scientific instruments. In spite of the five years of delay, Astro-E2 is still powerful and timely X-ray mission, because of the high energy resolution spectroscopy (FWHM 6 eV in 0.3–10 keV) and high-sensitivity wide-band spectroscopy (0.3–600 keV). The NeXT (New X-ray Telescope) mission, which we propose to have around 2010, succeeds and extends the science which Astro-E2 will open. It will carry five or six sets of X-ray telescopes which utilize super-mirror technology to enable hard X-ray imaging up to 60–80 keV. In mid-2010s, we would participate in the European XEUS mission, which explores the early (z>5) “hot” universe.     

N2O4真空排放试验研究

真空状态对高空液体火箭发动机的工作过程具有重要影响,研究液体火箭发动机高空点火、真空排放等过程时,必须对所采用的推进剂在真空状态与地面状态下的差别进行仔细研究。本文以某型高空发动机的真空排放过程为研究对象,根据排放管路中流速相等和流动时间相等的原则,设计了缩尺试验件,对N_2O_4真空排放过程进行了试验研究。结果表明,N_2O_4真空排放流量的轻微减少对发动机实际排放效果影响很小。