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Execution of the Spitzer in-orbit checkout and science verification plan

机译:执行Spittzer在轨道上结帐和科学验证计划

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The Spitzer Space Telescope is an 85-cm telescope with three cryogenically cooled instruments. Following launch, the observatory was initialized and commissioned for science operations during the in-orbit checkout (IOC) and science verification (SV) phases, carried out over a total of 98.3 days. The execution of the IOC/SV mission plan progressively established Spitzer capabilities taking into consideration thermal, cryogenic, optical, pointing, communications, and operational designs and constraints. The plan was carried out with high efficiency, making effective use of cryogen-limited flight time. One key component to the success of the plan was the pre-launch allocation of schedule reserve in the timeline of IOC/SV activities, and how it was used in flight both to cover activity redesign and growth due to continually improving spacecraft and instrument knowledge, and to recover from anomalies. This paper describes the adaptive system design and evolution, implementation, and lessons learned from IOC/SV operations.
机译:Spitzer Space Telescope是一个85厘米的望远镜,具有三种低温冷却仪器。推出后,在轨道结账(IOC)和科学验证(SV)阶段,初始化和委托科学业务初始化和委托,共计98.3天。 IOC / SV任务计划的执行逐步建立了Spitzer功能,考虑了热,低温,光学,指向,通信和操作设计和约束。该计划是以高效率进行的,使得有效地利用低温限量飞行时间。该计划成功的一个关键组成部分是IOC / SV活动时间表中的时间表储备的预先发布分配,以及由于不断改善航天器和仪器知识而涵盖活动重新设计和增长的航班中的使用方式。并从异常中恢复。本文介绍了从IOC / SV操作中吸取的自适应系统设计和演进,实现和经验教训。

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