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Progress on the Micro-X Rocket Payload

机译:Micro-X火箭有效载荷的进展

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The Micro-X High Resolution Microcalorimeter X-ray Imaging Rocket is a sounding rocket experiment that will combine a transition-edge-sensor x-ray-microcalorimeter array with a conical imaging mirror to obtain high-spectral-resolution images of extended and point x-ray sources. The target for Micro-X's first flight (slated for January 2011) is the Puppis A supernova remnant. The Micro-X observation of the bright eastern knot of Puppis A will obtain a line-dominated spectrum with up to 90,000 counts collected in 300 seconds at 2 eV resolution across the 0.3-2.5 keV band. Micro-X will utilize plasma diagnostics to determine the thermodynamic and ionization state of the plasma, to search for line shifts and broadening associated with dynamical processes, and seek evidence of ejecta enhancement. We describe the progress made in developing this payload, including the detector, cryogenics, and electronics assemblies. A detailed modeling effort has been undertaken to design a rocket-bourne adiabatic demagnetization refrigerator with sufficient magnetic shielding to allow stable operation of transition edge sensors, and the associated rocket electronics have been prototyped and tested.
机译:Micro-X高分辨率微热量计X射线成像火箭是一项探空火箭实验,它将结合过渡边缘传感器x射线微热量计阵列和圆锥形成像镜来获得扩展点x的高光谱分辨率图像-射线源。 Micro-X的首次飞行(定于2011年1月)的目标是Puppis A超新星残骸。对Puppis A明亮的东结的Micro-X观测将获得一条线为主的光谱,该光谱在300秒内以0.3到2.5 keV波段的2 eV分辨率收集了多达90,000个计数。 Micro-X将利用等离子体诊断程序来确定等离子体的热力学和电离状态,以寻找与动态过程相关的谱线移动和扩宽,并寻找喷射增强的证据。我们描述了开发这种有效载荷(包括探测器,低温装置和电子组件)所取得的进展。已经进行了详细的建模工作,以设计具有足够的磁屏蔽能力以使过渡边缘传感器稳定运行的火箭波绝热消磁制冷机,并且相关的火箭电子装置已经进行了原型设计和测试。

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