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Tungsten and Optics

机译:钨和光学

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The ESA INTErnational Gamma Ray Astrophysical Laboratory (INTEGRAL) satellite is the largest Gamma-Ray Astrophysics mission foreseen for this decade. Since its selection in 1994, three very innovative technologies were identified to achieve the INTEGRAL scientific goals: new generation Solid State Detectors, Active Veto Systems and Spatial Signal Multiplexing Systems. The high energy instruments of the mission, IBIS, SPI and JEM-X, have been developed by using the above referred technologies. The Grupo de Astronomia y Ciencias del Espacio (GACE) of the University of Valencia was chosen as the responsible to design and develop the Spatial Signal Multiplexing Systems (Coded Masks) for the three instruments, appointing the Spanish company SENER as the Prime Industrial Contractor. During the early design phase (1994-96) different materials were considered to modulate the high energy signals. Tungsten was selected as the optimum material for implementing the codes due to both its high density and large atomic number that provide the required stopping power. Codes follow HURA and MURA patterns, being the total mass of W used of around 280 kg. The scope of this paper is to summarise the milestones of the development programme carried out from 1994 until now, once the Flight Models have been manufactured, tested, delivered and mounted on the INTEGRAL satellite at Alenia and CNES (Oct/Nov 2000). We pay special attention to describing the complex Masks Themoelastic Designs, involving W coupled to composites and Ti. Mask Assemblies stability was tested in a wide range of temperatures (-80℃ +40℃) and mechanical stress (12g) at INTA facilities for Flight Qualification.
机译:ESA国际伽马射线天体物理实验室(INTEGRAL)卫星是近十年来最大的伽马射线天体物理学任务。自从1994年被选中以来,已经确定了三种非常创新的技术来实现INTEGRAL的科学目标:新一代固态检测器,有源否决系统和空间信号多路复用系统。特派团的高能仪器IBIS,SPI和JEM-X是使用上述技术开发的。瓦伦西亚大学的天文台和西班牙国家广播电视台(GACE)被选为负责为这三款仪器设计和开发空间信号多路复用系统(编码掩码)的负责人,并任命西班牙SENER公司为主要工业承包商。在早期设计阶段(1994-96年),考虑使用不同的材料调制高能信号。由于钨的高密度和大原子序数提供了所需的制动力,因此钨被选为实施该规范的最佳材料。代码遵循HURA和MURA模式,即所使用的W的总质量约为280 kg。本文的范围是总结从1994年到现在的飞行计划的里程碑,一旦飞行模型在Alenia和CNES的INTEGRAL卫星上被制造,测试,交付和安装(2000年10月/ 11月)。我们特别注意描述涉及W耦合到复合材料和Ti的复杂的面罩热弹性设计。在INTA设施进行的飞行资格测试中,面罩组件的稳定性在各种温度(-80℃+ 40℃)和机械应力(12g)下进行了测试。

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