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Advanced Geosynchronous Studies Imager thermal design

机译:先进的地球同步研究成像仪热设计

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Abstract: The AGSI instrument contains four focal plane arrays (FPAs) including the long wave IR (LWIR), medium wave IR (MWIR), short wave IR (SWIR), and the visible (VIS) FPA. The LWIR and MWIR FPAs are housed in a dewar. The SWIR FPA is housed in a separate dewar. The visible FPA will be located outside of the dewar. The AGSI instrument thermal subsystem is required to maintain the LWIR and MWIR FPAs at 65K, the SWIR FPA at 210 K, and the visible FPA between 210 K and 300 K. The stability of all four FPAs must be $POM 0.1 degrees C. The remainder of the optical system, telescope structure and instrument electronics must be maintained between 0 degrees C and 40 degrees C. Telescope alignment must also be maintained through the cooldown of the instrument optical bench, and during the diurnal and seasonal variations in orbital environment. The thermal design will accommodate such directly in the field-of-view for short periods of time without damage to the instrument, and with the ability to recover science operation quickly. This paper will discuss the thermal design needed to achieve these goals as well as detail the cryocooler and solar intrusion issues. !2
机译:摘要:AGSI仪器包含四个焦平面阵列(FPA),包括长波IR(LWIR),中波IR(MWIR),短波IR(SWIR)和可见光(VIS)FPA。 LWIR和MWIR FPA位于杜瓦瓶中。 SWIR FPA位于单独的杜瓦瓶中。可见的FPA将位于杜瓦瓶之外。需要使用AGSI仪器热子系统将LWIR和MWIR FPA维持在65K,将SWIR FPA维持在210 K,将可见FPA维持在210 K至300 K之间。所有四个FPA的稳定性必须为$ POM 0.1摄氏度。光学系统的其余部分,望远镜结构和仪器电子设备必须保持在0摄氏度至40摄氏度之间。还必须通过仪器光学工作台的冷却以及在轨道环境的昼夜变化中保持望远镜的对准。热设计将在短时间内直接将其容纳在视场中,而不会损坏仪器,并具有快速恢复科学运行的能力。本文将讨论实现这些目标所需的热设计,并详细介绍低温冷却器和太阳能入侵问题。 !2

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