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XMM-NEWTON Thermal Design and In-orbit Performance

机译:XMM-NEWTON热设计和在轨性能

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The XMM-NEWTON satellite is the ESA X-ray spaceborne observatory covering the soft X-ray portion of the electromagnetic spectrum. XMM-NEWTON has been put in orbit on December, 10~th 1999 by an Ariane 5 single launch. The spacecraft has a conventional thermal design that takes full advantage of he stable environment provided by its high altitude/long period orbit and by the limited variation of solar attitude angles in order to provide a stable plat from for the telescope system. The precise geometry and alignment of the telescope system impose strict temperature requirements so that not only temperature gradients have to be kept small but also, and more importantly, time-variations of the gradients have to be minimised. In verified by its thermal test programme is compared with the early in-orbit temperature measurements.
机译:XMM-NEWTON卫星是ESA X射线太空观测站,覆盖电磁频谱的软X射线部分。 XMM-NEWTON于1999年12月10日至10日由Ariane 5单发射升入轨道。航天器具有常规的热设计,充分利用了其高海拔/长周期轨道以及太阳姿态角的有限变化所提供的稳定环境,从而为望远镜系统提供了稳定的平台。望远镜系统的精确几何形状和对准要求严格的温度要求,因此不仅必须使温度梯度保持较小,而且更重要的是,必须使梯度的时间变化最小。在通过其热测试程序验证后,可与早期在轨温度测量结果进行比较。

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