异型封闭腔辐射几何学问题

讨论了解决异型封闭腔辐射几何学问题的几种方法:异型封闭腔内,表面间可见性的判断方法;优化异型封闭腔角系数计算的方法;确定异型封闭腔内定向辐射的壁面辐射源的方法.计算了两种结构喷管封闭腔内的角系数,并从角系数的互换性和完整性定理验证了方法的正确性和有效性,为异型封闭腔的辐射计算解决了几何问题.     

卫星红外辐射场理论模拟

在红外辐射场理论建模通用框架研究成果的基础上,对卫星的几何构型进行建模;通过背景辐射的非均匀化考虑,根据相应的物理模型对卫星温度场和红外辐射场进行了模拟计算,得到了卫星外表温度场和红外辐射场分布。     

普郎克定律的一个新推论

根据热辐射基本定律———普郎克定律,推导出了一个新的推论。即对于任意温度T的黑体辐射源,总存在一对应波长λδ,该波长对应的黑体单色辐射亮度对温度T的偏导数最大,且λδT =2 4 10 .3μm·K。这一结论对于单波长辐射温度计设计中探测器波段的选择有重要参考价值,根据此结论可以推出温度测量灵敏度最高的波长。     

武装直升机红外辐射计算中多重遮挡处理

针对武装直升机红外辐射计算中任意方向上可视净面积求取问题,提出了一种基于随机模拟的遮挡处理方法.该方法利用曲面造型方法建立直升机的三维模型,并将其离散为四边形面元,采用翼边拓扑结构描述直升机外形的数学模型.在此基础上,基于可见性测试、深度测试和遮挡测试原理对空间多边形面元进行遮挡判断,求出其遮挡面元集,再利用随机变量的统计方法对该多边形进行遮挡计算,求得净面积.对某型武装直升机和简单形体的计算表明,通过合理划分面元数和选取随机点数, 简单目标计算误差可以控制在5%以内,复杂目标可以控制在工程精度要求内.该方法已应用于武装直升机红外辐射特性计算软件中,应用表明该方法稳定、可靠,适于工程分析.      

假目标诱骗对抗反辐射导弹作战效能分析

研究多个假目标保护一个真目标(雷达)对抗反辐射导弹(ARM)的作战效能.在确定ARM瞄准方向的基础上,给出导引头在分辨目标时刻对真假目标截获概率的计算方法;推导出计算真目标受到ARM多次攻击时被杀伤概率的通用公式.研究结果表明:在评估假目标诱骗对抗ARM的效能时,必须考虑目标损失积累的影响;为提高诱骗效能,在增加假目标数量的同时,应降低其易损性,提高发射功率,并采用合理的布局方案.     

二次包封CMOS器件电子辐照实验研究

对CMOS器件54HCT00进行了复合材料的二次包封，研制了试验电路板，在器件加电工作下进行电子辐照试验的动态测试．结果表明，二次封装的器件抗总剂量的能力提高了1—2个数量级，得到了预期的数据和结果．这些工作为商用器件的空间开拓使用提供了很好的途径．     

A 3NM-64_He added to LARC for Solar Extreme Event studies during solar cycle 24

The Antarctic Laboratory for Cosmic Rays (LARC, acronym for Laboratorio Antartico per i Raggi Cosmici or Laboratorio Antártico para Rayos Cósmicos) operates on King George Island (South Shetlands). Since January 1991 a standard 6NM-64 detector has been recording continuous cosmic ray measurements and several Ground-Level Enhancements have been registered. Here we describe the different phases performed in Italy for the realization of a 3NM-64_³He detector, which started its measurements during the Italian XXII Antarctic Summer Campaign. Data recorded during solar activity cycle 24 will furnish an useful research tool for the next Solar Extreme Events.     

Coronal fast wave trains of the decimetric type IV radio event observed during the decay phase of the June 6, 2000 flare

The 22 min long decimetric type IV radio event observed during the decay phase of the June 6, 2000 flare simultaneously by the Brazilian Solar Spectroscope (BSS) and the Ond?ejov radiospectrograph in frequency range 1200–4500 MHz has been analyzed. We have found that the characteristic periods of about 60 s belong to the long-period spectral component of the fast wave trains with a tadpole pattern in their wavelet power spectra. We have detected these trains in the whole frequency range 1200–4500 MHz. The behavior of individual wave trains at lower frequencies is different from that at higher frequencies. These individual wave trains have some common as well as different properties. In this paper, we focus on two examples of wave trains in a loop segment and the main statistical parameters in their wavelet power and global spectra are studied and discussed.     

Relativistic electron fluxes and dose rate variations during April–May 2010 geomagnetic disturbances in the R3DR data on ISS

Space radiation has been monitored successfully using the Radiation Risks Radiometer-Dosimeter (R3D) installed at the ESA EXPOSE-R (R3DR) facility outside of the Russian Zvezda module of the International Space Station (ISS) between March 2009 and January 2011. R3DR is a Liulin type spectrometer–dosimeter with a single Si PIN detector 2 cm² of area and 0.3 mm thick. The R3DR instrument accumulated about 2 million measurements of the absorbed dose rate and flux of 10 s resolution. The total external and internal shielding before the detector of R3DR device is 0.41 g cm⁻². The calculated stopping energy of normally incident particles to the detector is 0.78 MeV for electrons and 15.8 MeV for protons. After the Coronal Mass Ejection (CME) at 09:54 UTC on 3 April 2010, a shock was observed at the ACE spacecraft at 0756 UTC on 5 April, which led to a sudden impulse on Earth at 08:26 UTC. Nevertheless, while the magnetic substorms on 5 and 6 of April were moderate; the second largest in history of GOES fluence of electrons with energy >2 MeV was measured. The R3DR data show a relatively small amount of relativistic electrons on 5 April. The maximum dose rate of 2323 μGy day⁻¹ was reached on 7 April; by 9 April, a dose of 6600 μGy was accumulated. By the end of the period on 7 May 2010 a total dose of 11,587 μGy was absorbed. Our data were compared with AE-8 MIN, CRESS and ESA-SEE1 models using SPENVIS and with similar observations on American, Japanese and Russian satellites.     

PHITS simulations of the Protective curtain experiment onboard the Service module of ISS: Comparison with absorbed doses measured with TLDs

“Protective curtain” was the physical experiment onboard the International Space Station (ISS) aimed on radiation measurement of the dose – reducing effect of the additional shielding made of hygienic water-soaked wipes and towels placed on the wall in the crew cabin of the Service module Zvezda. The measurements were performed with 12 detector packages composed of thermoluminescent detectors (TLDs) and plastic nuclear track detectors (PNTDs) placed at the Protective curtain, so that they created pairs of shielded and unshielded detectors.