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本文分析了宇航用精密恒温箱设计,并通过工程实践、实测数据,证实了该设计满足宇航设备中晶体振荡器频率稳定性的温控要求。
In this paper, the design of space thermostat for aerospace is analyzed, and the temperature control requirements of the design to meet the frequency stability of crystal oscillator in aerospace equipment are confirmed through engineering practice and measured data.