论文标题
射线追踪软X射线极化法的小轨道任务
Ray-tracing a small orbital mission for soft-X-ray polarimetry
论文作者
论文摘要
X射线极化学仍然是未知的领域。随着IXPE即将推出的,我们将在2 KEV以上的Energies上了解更多有关X射线两极分化的信息,但是到目前为止,目前或公认的任务尚无2 KEV以下的观察能力。我们为小型轨道任务提供了射线追踪结果,该成果可以在NASA的先驱或SmallSat成本额定限制中启动,以在2 KEV以下提供X射线极化法。该设计基于使用横向毕业的多层(ML)镜子的使用,这是我们在理论上为Redsox polarimeter开发的概念,为此,大多数组件都在实验室中得到了验证。在这项贡献中,我们根据相同的想法描述了一个单个渠道轨道任务,但根据独特的成本和空间要求进行了修改。所有结果都很容易扩展到两个或多个偏光仪通道。扩大规模只会增加有效区域,并减少旋转仪器以测量不同极化方向的需求。特别是,我们使用射线轨迹来定义分散光栅的最大尺寸并确定一致性预算。
X-ray polarimetry is still largely uncharted territory. With the upcoming launch of IXPE, we will learn a lot more about X-ray polarization at energies above 2 keV, but so far no current or accepted mission provides observational capabilities below 2 keV. We present ray-tracing results for a small orbital mission that could be launched within NASA's Pioneer or SmallSat cost-cap to provide X-ray polarimetry below 2 keV. The design is based on the use of laterally-graded multi-layer (ML) mirrors, a concept that we have developed theoretically for the REDSoX Polarimeter, for which most components have been verified in the laboratory. In this contribution, we describe a single channel orbital mission based on the same idea, but modified to the unique cost and space requirements. All results scale up easily to two or more polarimetry channels. Scaling up would simply increase the effective area and reduce the need to rotate the instrument to measure the different polarization directions. In particular, we use the ray-traces to define the maximum size of the dispersion gratings and to determine an alignment budget.