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Significance of Nonequilibrium Surface Interactions in Stardust Return Capsule Ablation Modeling

机译:非平衡表面相互作用在星尘返回胶囊消融建模中的意义

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The gas-surface modeling of high-density materials exposed to high-pressure atmospheric reentry conditions was extended to include low-density materials interacting with low-pressure atmospheric conditions. The fully implicit ablation thermal response code and multicomponent ablation thermochemistry program were extended to include nonequilibrium surface conditions for the Stardust return capsule. The Stardust return capsule reentered Earth's atmosphere experiencing low pressure and had a low-density heat shield material. The material response of the Stardust return capsule was previously only modeled with surface equilibrium. Validation against Stardust reentry flight data showed that the equilibrium assumption led to an overprediction of recession and that the inclusion of nonequilibrium reduced the overprediction of this parameter. Incorporating the Park finite rate model nonequilibrium surface conditions led to a reduction in the calculated value of recession at the stagnation point from 1.12 to 0.72 cm in a nominal simulation of the Stardust return capsule. The nonequilibrium recession was closer to the measured recession of 0.65 cm. Incorporating nonequilibrium conditions also decreased the calculated total heat load from 28 to 19 kJ/cm~2. The improved material response method is applicable to a range of reentries, including future missions such as the Orion crew exploration vehicle.
机译:扩展了暴露于高压大气折返条件下的高密度材料的气体表面模型,以包括与低压大气条件相互作用的低密度材料。完全隐含的消融热响应代码和多组分消融热化学程序已扩展为包括星尘返回胶囊的非平衡表面条件。星尘返回舱重新进入了处于低压状态的地球大气层,并具有低密度的隔热罩材料。星尘返回舱的物质响应以前仅使用表面平衡建模。对星尘再入飞行数据的验证表明,均衡假设导致经济衰退的过度预测,而非均衡的纳入减少了该参数的过度预测。结合Park有限速率模型的非平衡表面条件,导致在星尘返回舱的名义模拟中,停滞点的衰退计算值从1.12厘米降低到0.72厘米。非平衡衰退更接近测得的0.65厘米衰退。引入非平衡条件也将计算出的总热负荷从28 kJ / cm〜2降低到19 kJ / cm〜2。改进的材料响应方法适用于多种重入,包括未来的任务,例如猎户座乘员探索车。

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