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In this paper, based on the analysis of the thermal environment where the space target embeds and the study of thermal exchanges between the environment and the space target, the mathematics model of the temperature field for the space target is present by using the thermal network method. The temperature and radiant flux of the target surface are calculated, the characteristic of the distribution of temperature and IR radiation from the space target is discussed in detail. 相似文献
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红外双色复合仿真系统测温技术研究 总被引:1,自引:1,他引:0
为了模拟红外制导时目标和干扰的等效辐射环境,并比较单色测温和比色测温两种方法在复杂环境下目标测温效果的差异,利用红外双色复合仿真系统对空间6 km处目标和干扰弹进行了实物模拟.通过准确标定的热像仪,采用单色和比色测温两种方法对不同温度的目标和干扰进行测试.利用经标定的中波热像仪和长波热像仪对黑体测温,黑体温度为(20~60)℃时,长波热像仪的绝对误差限为0.5 ℃;黑体温度为(50~120) ℃时,中波热像仪的绝对误差限为0.2 ℃.当目标温度为500 ℃、干扰温度为1 000 ℃时,用长波红外、中波红外、比色方法测得的目标温度分别为28.5 ℃、148.3 ℃、322.4 ℃,干扰温度分别为56.7 ℃、223.2 ℃、660.1 ℃.实验结果表明,在复杂环境下采用比色测温方法更能真实反映目标的温度特性. 相似文献
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We have examined the implosion of an indirectly driven reentrant-cone shell target to clarify the issues attendant on compressing fuel for a fast ignition target. The target design is the hydrodynamic equivalent of a NIF cryoignition target scaled to be driven by Omega. Implosions were imaged with backlit x radiographs and modeled with LASNEX. The simulations were generally in good agreement with the experiments with respect to the shell diameter, density, and symmetry, but did not show the prestagnation central absorption maximum. The existence of material between the original cone and the shell is sensitive to gold M-band radiation, which penetrates the shell and ablates gold from the cone. The simulated radiographs using recently measured M-band fractions showed absorption between the cone and shell similar to the experiment. This gold ablation might be a problem in a cryoignition target. 相似文献
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根据空间应用电子设备的热控要求,对空间光学遥感器的控制电箱进行了热控设计。首先,总结了空间电子设备的热设计原则。针对空间光学遥感器控制电箱介绍了相应的热设计流程,对典型的大功率器件进行了温差推算,并说明了电箱的各电路板和大功率元器件的热设计方案。最后,通过热分析和热试验手段对热控电箱的热控方案进行了验证。试验结果表明:控制电箱的整机稳态工况热平衡温度小于30℃,各元器件的最高壳温在54.2℃以内。结果验证了该设计方案完全满足设计指标要求。 相似文献
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空间相机接触热阻的计算 总被引:2,自引:0,他引:2
为了解决空间相机接触热阻难以确定的问题,从接触面传导和辐射换热的角度考虑,给出了其接触热阻的计算方法。根据空间相机的材料、加工、装配及其特殊运行环境,得到一个合理的接触系数范围。以空间相机的正视相机为例,对其结构进行合理的简化,利用I-DEAS/TMG热分析模块建立有限元模型,仿真计算了低温稳态平衡工况,考查了热阻波动对温度分布的影响。正视相机热分析计算结果和热环境模拟试验数据较为吻合,最大偏差为0.45℃。研究结果表明,该接触热阻计算方法合理,可以预测太空环境中干接触的精密加工表面间的接触热阻。 相似文献
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Lei AL Tanaka KA Kodama R Kumar GR Nagai K Norimatsu T Yabuuchi T Mima K 《Physical review letters》2006,96(25):255006
We propose a foam cone-in-shell target design aiming at optimum hot electron production for the fast ignition. A thin low-density foam is proposed to cover the inner tip of a gold cone inserted in a fuel shell. An intense laser is then focused on the foam to generate hot electrons for the fast ignition. Element experiments demonstrate increased laser energy coupling efficiency into hot electrons without increasing the electron temperature and beam divergence with foam coated targets in comparison with solid targets. This may enhance the laser energy deposition in the compressed fuel plasma. 相似文献
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为了使空间相机热设计、热分析、热试验具备准确、可靠的热边界条件,对太阳同步圆轨道空间相机的瞬态外热流进行了计算。总结了卫星空间定位的6个轨道根数之间的关系,给出了太阳同步圆轨道空间定位的必要参数。针对某给定太阳同步圆轨道,采用STK软件进行了轨道面与太阳光矢量相对位置关系(β角)的计算,确定了该轨道的高、低温工况位置。归纳了空间外热流的理论计算方法,以外接于卫星平台的空间相机为例,建立了外热流计算模型,采用IDEAS/TMG模块对给定太阳同步圆轨道的高、低温工况轨道周期内瞬态外热流变化进行了分析计算,得出了太阳辐射热流、地球太阳反照热流、地球红外辐射热流在轨道周期内的详细变化曲线,得到的结果可以作为空间相机热设计、热分析及地面热试验外热流模拟的输入条件。 相似文献
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K. Mima K. A. Tanaka R. Kodama T. Johzaki H. Nagatomo H. Shiraga N. Miyanaga M. Murakami H. Azechi M. Nakai T. Norimatu K. Nagai T. Taguchi H. Sakagami 《The European Physical Journal D - Atomic, Molecular, Optical and Plasma Physics》2007,44(2):259-264
Reviewed are the present status of the fast ignition researches. Since
1997, the fast ignition experiment and theory researches have been
extensively continued at the Institute of Laser Engineering of Osaka
University. In particular, the cone-shell target experiments and simulation
research have been progressing. In order to demonstrate heating of imploded
high density plasma to the ignition temperature, in the April of 2003, the
construction of heating laser of 10 kJ/10 ps/1.06 μm (Laser for Fusion
Experiment; LFEX), for FIREX-I (Fast Ignition Realization Experiment) has
started. The fabrication of DT foam cryogenic cone target is also under
development as a collaboration program between Osaka University and NIFS (National Institute for Fusion Science). The LFEX
will be completed in 2008.
After the completion of LFEX, the foam cryogenic cone shell target
experiment will start in 2008. As a new approach toward a compact ignition,
an impact fusion has been proposed, where the ablative acceleration to the
order of 108 cm/s is the key issue. The ablation acceleration related
to the impact fusion has been explored by experiments. 相似文献
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Jobin K. Antony Gurneesh Singh Jatana Nilesh J. Vasa V. L. N. Sridhar?Raja A. S. Laxmiprasad 《Applied Physics A: Materials Science & Processing》2010,101(1):161-165
Laser Induced Breakdown Spectroscopy (LIBS) can be considered as a prominent technology for compositional analysis of materials
in low-pressure space applications. In space applications, usually LIBS is conducted in a low-pressure environment and proper
understanding of the plasma parameters is significant for any improvement in the system. A model is developed to describe
the heating and subsequent melting, vaporization and ionization of a target material during LIBS process. A numerical model
based on one-dimensional thermal conductivity equation is being used to simulate the target evaporation and a hydrodynamic
model is used to simulate plume expansion. Further, an experimental approach of measuring spectral emission from the ablation
plume using emission spectroscopy and estimating the plasma state, such as the ionization species, and average plasma temperature,
is investigated. An important result of this work is that for different ambient conditions, laser ablation plume dynamics
can be estimated. 相似文献
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为了研究阴极微凸起形状对其热不稳定性的影响,采用数值模拟方法研究了不同外加电场条件下,圆柱、圆台和圆锥形等不同形状微凸起的热不稳定性发展过程。结果显示:对于不同形状的微凸起,当微凸起顶部温度达到阴极材料的熔点时,微凸起内部温度分布差异显著,随着微凸起形状由圆柱-圆台-圆锥形变化,微凸起内部温度接近材料熔点的部位越来越少;外加电场相同时,微凸起形状越接近圆锥形,爆炸电子发射延迟时间越长;在阴极表面电场强度高于11 GV/m时,爆炸电子发射延迟时间随着微凸起顶底半径比值的减小或阴极表面电场强度的下降近似成指数规律增长。 相似文献
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为了检测航天相机主动热控系统的功能、性能及可靠性,设计了主动热控仿真测试系统。依据传热学基本定律、航天器轨道理论和热控策略,给出了计算航天相机温度场的热网络数学模型,使主动热控系统能在模拟的空间热环境中连续工作,实现了对主动热控系统的闭环仿真测试。采用两个数字电位器相串联的方法模拟温度传感器的走势,得到的最大阻值为100 kΩ,精度达到10Ω,符合设计中对总电阻和电阻变化率的需求,实现了对主动热控系统的功能、性能以及可靠性的仿真测试。 相似文献
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为了验证空间光学系统热设计的合理性,利用光-机-热集成的热光学分析技术论证了空间光学系统的热设计方案。首先,阐述了热光学技术的一般方法以及热光学技术与热设计的关系,同时根据空间光学遥感器所处的空间环境和结构特点,应用被动和主动热控技术对空间光学系统进行了热设计。然后,利用有限元方法对热控后的温度场和热弹性变形进行了分析,得出该温度载荷条件下光学元件表面的变形量及刚体位移量,利用Zemike多项式进行了波面拟合。最后,用CodeV光学设计软件计算了热载荷作用下光学系统的传递函数。结果表明,各种工况下全视场范围内光学系统分辨率为50lp时,传递函数均超过0.5,成像良好,能够满足光学设计指标,热设计方案合理可行。 相似文献
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把落到目标上的总的环境辐射等效成一个温度为T0的黑体辐射,研究了环境辐射改变时对热成象系统灵敏度方程的影响,从而从理论上证明了用改变环境辐射的办法可以测定目标的比辐射率。给出了用红外测温仪测定环境等效黑体温度T0的方法和实验结果。给出了用红外测温仪测定目标比辐射率的一种新方法及实验结果。对于环境辐射不能忽略时如何用比辐射计测定目标的真实温度作了方法性和原理性的讨论。对于如何用测温仪测定地物对太阳的光谱反射率也作了方法性和原理性的讨论。
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