基于参数化积分软目标的可重复使用运载火箭热防护系统建模方法

A. Aprovitola, L. Iuspa, A. Viviani
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引用次数: 2

摘要

本文研究了概念可重复使用运载火箭热防护系统的建模过程。采用一种新的参数化模型,该模型基于由一组软物体原语创建的标量场,用于在车辆表面分配几乎任意的无缝绝缘材料分布。使用合适的几何支撑创建软物体的大聚集体,允许使用有限数量的参数分布涂层材料。应用于不同概念车辆配置的指定厚度图和材料布局显示了模型的灵活性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Parametric Integral Soft Objects-based Procedure for Thermal Protection System Modeling of Reusable Launch Vehicle
The present paper deals with a modeling procedure of a thermal protection system (TPS) designed for a conceptual reusable launch vehicle (RLV). A novel parametric model based on a scalar field created by a set of soft object primitives is used to assign an almost arbitrary seamless distribution of insulating materials over the vehicle surface. Macroaggregates of soft objects are created using suitable geometric supports allowing a distribution of coating materials using a limited number of parameters. Applications to different conceptual vehicle configurations of an assigned thickness map and materials layout show the flexibility of the model.
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