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191.
气象卫星扫描辐射计的辐射定标   总被引:2,自引:0,他引:2  
阐述了气象卫星扫描辐射计的辐射定标。包括卫星发射前的地面定标,飞行中的星上定标及星地对比定标。指出飞行中的可见光波段的定标至今还未能投入业务使用,仍处于研究阶段,而静止气象卫星的飞行中定标,无论红外或是可见光波段只能做到相对定标。为解决绝对定标问题,必须寻求星体外的客观目标作为定标源。采用这一途径,即使星上定标设备失效,也不致影响卫星数据的使用。  相似文献   
192.
6mm,8mm,13mm辐射计校准系统的研制   总被引:3,自引:0,他引:3  
为解决相应频段的辐射计的灵敏度、线性度、稳定性的定标问题.叙述了6mm,8mm,13mm辐射计校准系统的主要技术问题,给出了技术指标,系统组成,工作原理,校准结果及不确定度分析.该系统在国内首次将变温标准辐射源用于辐射计校准,有广泛的应用前景.  相似文献   
193.
介绍了适用于红外焦平面成像探测辐射特性测量的3种典型标定方案,推导了3种方案对应的单像元辐射通量公式,并在此基础上分析了3种方案对黑体温度的需求。对3种方案的优缺点进行了综合比较,对特殊应用场合的标定方案提出了建议。  相似文献   
194.
Whipple防护结构超高速撞击极限分析   总被引:1,自引:0,他引:1  
丁莉  庞宝君  张伟 《强度与环境》2006,33(2):12-16,22
空间碎片的超高速撞击可能导致航天器发生严重的损伤甚至灾难性的失效,由于近地轨道上空间碎片的增加导致航天器的安全受到严重威胁,必须设置防护结构予以防护。本文从动力学分析入手,初步建立超高速撞击时Whipple防护结构的撞击极限方程,得到了与撞击极限相关的参数以及参数之间的关系,为实验提供基础。本文方程得到的撞击极限曲线与已有方程的撞击极限曲线吻合较好。  相似文献   
195.
本文提出一种基于混响室平台将电磁环境和自然环境结合的综合试验箱集成技术,该试验箱集成了环境试验条件和电磁辐射敏感度试验条件,可以在高低温、湿热、温度循环、温度冲击等多种环境条件下同时对电子设备施加电磁辐射干扰,考核电子设备在同施加环境应力和电磁应力的复杂条件下的适应性。经过设计、建造和测试,该集成技术满足各项预期指标并容易进行推广,可进一步降低设备试验成本。  相似文献   
196.
197.
The aim of the present paper is to study the numerical solutions of the steady MHD two dimensional stagnation point flow of an incompressible nano fluid towards a stretching cylinder.The effects of radiation and convective boundary condition are also taken into account.The model used for the nanofluid incorporates the effects of Brownian motion and thermophoresis.The resulting nonlinear momentum,energy and nano particle equations are simplifed using similarity transformations.Numerical solutions have been obtained for the velocity,temperature and nanoparticle fraction profles.The influence of physical parameters on the velocity,temperature,nanoparticle fraction,rates of heat transfer and nanoparticle fraction are shown graphically.  相似文献   
198.
Radiation exposure in space is expected to increase the risk of cancer and other adverse biological effects in astronauts. The types of space radiation of particular concern for astronaut health are protons and heavy ions known as high atomic number and high energy (HZE) particles. Recent studies have indicated that carcinogenesis induced by protons and HZE particles may be modifiable. We have been evaluating the effects of proton and HZE particle radiation in cultured human cells and animals for nearly a decade. Our results indicate that exposure to proton and HZE particle radiation increases oxidative stress, cytotoxicity, cataract development and malignant transformation in in vivo and/or in vitro experimental systems. We have also shown that these adverse biological effects can be prevented, at least partially, by treatment with antioxidants and some dietary supplements that are readily available and have favorable safety profiles. Some of the antioxidants and dietary supplements are effective in preventing radiation induced malignant transformation in vitro even when applied several days after the radiation exposure. Our recent progress is reviewed and discussed in the context of the relevant literature.  相似文献   
199.
The equilibrium temperature of a system in space can be lowered by a suitable choice of its geometry and its attitude. This remark is important for devices based on medium temperature and high temperature superconducting materials, and offers the possibility of their fully passive cooling without or with a marginal recourse to active systems. General parameterizations are given and simple schemes discussed. The adopted geometrical configuration and the attitude can enhance the role of passive cooling of the large superconducting magnetic systems required for protecting from ionizing radiation manned habitats in deep space. A specific example based on MgB2 cable for protecting large volume habitats (500 and 1000 m3) is treated. The systems can be run in deep space at equilibrium temperatures around 20 K mainly by passive cooling, provided that their geometry and attitude would be suitably chosen.  相似文献   
200.
Measurements taken in Low Earth Orbit (LEO) onboard the International Space Station (ISS) and transit vehicles have been extensively used to validate radiation transport models. Primarily, such comparisons were done by integrating measured data over mission or trajectory segments so that individual comparisons to model results could be made. This approach has yielded considerable information but is limited in its ability to rigorously quantify and differentiate specific model errors or uncertainties. Further, as exploration moves beyond LEO and measured data become sparse, the uncertainty estimates derived from these validation cases will no longer be applicable. Recent improvements in the underlying numerical methods used in HZETRN have resulted in significant decreases in code run time. Therefore, the large number of comparisons required to express error as a function of a physical quantity, like cutoff rigidity, are now possible. Validation can be looked at in detail over any portion of a flight trajectory (e.g. minute by minute) such that a statistically significant number of comparisons can be made. This more rigorous approach to code validation will allow the errors caused by uncertainties in the geometry models, environmental models, and nuclear physics models to be differentiated and quantified. It will also give much better guidance for future model development. More importantly, it will allow a quantitative means of extrapolating uncertainties in LEO to free space. In this work, measured data taken onboard the ISS during solar maximum are compared to results obtained with the particle transport code HZETRN. Comparisons are made at a large number (∼77,000) of discrete time intervals, allowing error estimates to be given as a function of cutoff rigidity. It is shown that HZETRN systematically underestimates exposure quantities at high cutoff rigidity. The errors are likely associated with increased angular variation in the geomagnetic field near the equator, the lack of pion production in HZETRN, and errors in high energy nuclear physics models, and will be the focus of future work.  相似文献   
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