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The new operational strategy for XMM-Newton's tank thermal control, after Low Temperature Protection thermostat failure

机译:低温保护恒温器故障后,XMM-Newton储罐热控制的新操作策略

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During the Eclipse season in July 2009, XMM-Newton had a failure on a Low Temperature Protection (LTP) thermostat in the heater circuit for the thermal control of the Tank 1 of the Spacecraft, and its temperature dropped down to 21.25 degC, below the nominal threshold of 24.6 degC. The Reaction Control System of XMM-Newton is based on 4 tanks connected in series to feed the main one (Tank 1) with pressurized gas, and a temperature gradient among the tanks could cause fuel migration between the tanks and in the worst case, if the main tank is emptied, this in turn can lead to gas bubble ingestion in the pipes downstream feeding the thrusters. The main tank temperature is now controlled by means of uplinking a duty cycle to the Transistor Switch (TSW), connected in parallel to the failed LTP thermostat, and manually reacting to any temperature deviation outside the nominal range. This duty cycle is implemented via Time Tagged Commands which are generated on ground following an operational strategy that has to take into account safety issues and contingency situations. The thermal cycle for the Tank 1 is variable because it depends on the attitude, the position in the orbit and the season, therefore it can not be easily predicted. The strategy adopted is an adjustment of the thermal cycle to be done every revolution, based on the previous one, changing the time of activation and deactivation of the TSW. The operation is implemented in three different layers: ⅰ) an automated script to calculate the time of the Time Tags in order to correct the thermal cycle; ⅱ) a procedure to calculate manually the Time Tags in case automation fails, and ⅲ) an Operational Instruction for the Spacecraft Controller to operate the TSW in case the temperature goes out of the nominal range. This paper describes the failure suffered by XMM-Newton and the following operational strategy adopted to cope with the failure.
机译:在2009年7月的Eclipse季节,XMM-Newton的加热回路中的低温保护(LTP)温控器发生故障,用于对航天器Tank 1进行热控制,其温度下降至21.25摄氏度,低于标称阈值为24.6摄氏度。 XMM-Newton的反应控制系统基于串联的4个油箱,向主油箱(油箱1)供入加压气体,并且油箱之间的温度梯度可能会导致油箱之间的燃料迁移,在最坏的情况下,如果主油箱已排空,这反过来会导致在向推进器供气的下游管道中吸入气泡。现在,通过将占空比上传至晶体管开关(TSW),并与故障LTP温控器并联连接,并对任何超出标称范围的温度偏差做出手动反应,来控制主油箱温度。该工作周期是通过时间标记命令实现的,该命令是根据一种必须考虑安全问题和应急情况的操作策略在地面上生成的。坦克1的热循环是可变的,因为它取决于姿态,在轨道上的位置和季节,因此不容易预测。采取的策略是在前一轮的基础上调整每次旋转要完成的热循环,从而改变TSW的激活和停用时间。该操作在三个不同的层中实现:ⅰ)一​​个自动脚本来计算时间标签的时间,以纠正热循环; ⅱ)在自动化失败的情况下手动计算时间标签的程序,ⅲ)在温度超出标称范围的情况下航天器控制器操作TSW的操作指令。本文介绍了XMM-Newton所遭受的故障以及为应对该故障而采取的以下操作策略。

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