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Compound Solar Sail with Optical Properties: Models and Performance

机译:具有光学特性的复合太阳帆:模型和性能

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A compound solar-sail model, in which the optical properties of the collector, reflector, and director have been taken into account, has been investigated. A compact expression for the resultant force acting on the sailcraft has been derived in which two force coefficients depend only on the optical properties of the reflecting material, whereas the third one also depends on the collector geometry. Unlike the ideal case, the sailcraft acceleration is different from zero for any cone angle. This new model allows one to establish a more realistic comparison between the performance attainable with conventional and compound solar sails. To this end, the optimal control law for minimum-time three-dimensional interplanetary trajectories has been solved using an indirect approach. The resulting steering law generalizes a similar result available for an ideal compound sail. Applications to transfers toward Mars and Venus have been discussed. Assuming that the main losses of the compound sail are concentrated in the collector, the minimum transfer times obtainable with a compound sail are shorter than those of a conventional sail with optical properties and are close to those of an ideal flat sail. As there exists a critical cone angle beyond which the sailcraft acceleration of the optical model is greater than that with an ideal model, even better performance of compound sails are expected for those missions requiring high values of cone angles. We finally note that a fully realistic comparison between conventional and compound solar sails needs a more detailed study. In fact, it is likely that the compound sail will have a significant mass penalty compared to a flat sail because of the mass of the additional mirrors and the structure required to join them together. An important issue would be to determine the payload mass delivered for a given launch mass, taking into account both trajectory optimization and the mass budget of the flat and compound sails. This is beyond the scope of the current Note and is left to future research.
机译:研究了复合太阳帆模型,其中考虑了集热器,反射器和指向矢的光学特性。已经得出了作用在帆船上的合力的紧凑表达式,其中两个力系数仅取决于反射材料的光学特性,而第三个系数也取决于收集器的几何形状。与理想情况不同,帆艇加速度在任何锥角下都不为零。这一新模型使人们可以在传统和复合太阳帆的性能之间建立更现实的比较。为此,使用间接方法解决了最小时间三维行星际轨道的最优控制律。由此产生的转向定律可概括出理想复合帆可用的类似结果。已经讨论了向火星和金星转移的应用。假设复合帆的主要损失集中在收集器中,则复合帆可获得的最短转移时间比具有光学特性的常规帆要短,并且与理想的平帆接近。由于存在一个临界锥角,超过该临界锥角,光学模型的航行器加速度将大于理想模型的航行器加速度,因此对于那些需要较高锥角值的任务,复合帆的性能有望更高。我们最终注意到,对常规太阳帆和复合太阳帆之间的完全现实的比较需要更详细的研究。实际上,由于附加镜的质量以及将它们连接在一起所需的结构,与平帆相比,复合帆可能会遭受重大的质量损失。一个重要的问题是要确定给定发射质量所输送的有效载荷质量,同时要考虑轨迹优化以及平帆和复合帆的质量预算。这超出了当前注释的范围,留待将来研究。

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