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Detailed investigation of spacecraft glow.

机译:对航天器发光的详细调查。

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The phenomenon of spacecraft glow is simulated in detail, using a three-step procedure. The goals of the study are defined.; Characteristics of the glow phenomenon are described. The experimental behavior of glow observed around several orbital vehicles and in ground-based laboratory experiments is described. Emissions from electrically-excited nitrogen dioxide is identified as the source of the glow. Examples of typical glow spectra are presented. An overview of the atmospheric characteristics at relevant altitudes is included.; The direct simulation Monte Carlo (DSMC) technique is described and resolution difficulties in simulating rare species and events are noted. Common approaches to overcoming resolution problems are outlined. The DSMC overlay technique is described along with its benefits and limitations. Specific attention is given to the accurate inclusion of rare chemical events.; The set of surface events to be simulated is defined and is described in differential form. A Runge-Kutta method is employed to solve the resulting differential equations. Modifications to the method to account for satellite rotation are described. A steady-state analysis of the system of equations is performed. The flux of emitted, excited nitrogen dioxide is calculated. An analytical model is used to calculate the brightness of glow based on this emitted flux.; Results from each stage of the solution procedure are analyzed. The flow field results are found to be typical of rarefied, hypersonic flow. The extreme non-equilibrium behavior of the flow is captured. The importance of chemical production at the lower altitudes is shown. A dependence of the surface concentrations on both the total and relative incident fluxes is observed. Critical surface events are identified via a sensitivity study. Comparison of the variation of glow brightness with experimental results is favorable. The trend is for the simulated results to overpredict the brightness. The agreement is poorer at the upper altitudes, due to greater uncertainties in the initial conditions. The importance of the ambient density of nitric oxide is shown.
机译:使用三步过程详细模拟了航天器辉光现象。确定了研究目标。描述了辉光现象的特征。描述了在几个轨道飞行器周围和地面实验室实验中观察到的辉光的实验行为。电激发的二氧化氮的排放被确定为辉光的来源。给出了典型的发光光谱的例子。包括有关海拔高度大气特征的概述。描述了直接模拟蒙特卡洛(DSMC)技术,并指出了模拟稀有物种和事件的解析难度。概述了解决分辨率问题的常用方法。描述了DSMC覆盖技术及其优点和局限性。特别注意稀有化学事件的准确纳入。定义了要模拟的一组表面事件,并以差分形式对其进行了描述。采用Runge-Kutta方法求解所得的微分方程。描述了解决卫星自转方法的修改。对方程组进行稳态分析。计算了发出的激发二氧化氮的通量。分析模型用于根据此发射通量计算辉光的亮度。分析了解决程序每个阶段的结果。发现流场结果是稀疏高超声速流的典型结果。捕获了流动的极端非平衡行为。显示了在低海拔地区化学生产的重要性。观察到表面浓度对总和相对入射通量的依赖性。通过敏感性研究确定了关键的表面事件。将发光亮度的变化与实验结果进行比较是有利的。趋势是模拟结果会过度预测亮度。由于初始条件的不确定性较大,该协议在高海拔地区较差。显示了一氧化氮的环境密度的重要性。

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