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小行星探测器电缆绝缘层高低温交变收缩验证方法

Verification Method for Shrinkage of Asteroid Probe Cable Insulation Under Alternating High and Low Temperatures

  • 摘要: 针对小行星探测器电缆在轨10年飞行阶段经受极端温度交变后可靠性、安全性的需求,耐温试验结果表明:经历高低温交变后电连接器内部导线根部绝缘层回缩导致线芯裸露,存在电气短路风险。本文提出了基于异速生长模型的导线端头绝缘层经历高低温交变后收缩的验证方法,通过地面试验数据构造导线绝缘层沿导线长度方向(轴向)的收缩量拟合曲线,对导线端头绝缘层经历多次极端温度交变后的收缩量进行预测,评估电缆两端导线根部的绝缘保护有效性。该方法可为深空探测领域极端温度交变环境下的电缆可靠性与安全性设计提供参考。

     

    Abstract: Aiming at the requirement of reliability and security of the cables of asteroid exploration spacecraft which experience extreme temperature alternations many times during long-term in-orbit flight, the results of temperature resistance experiment show that the conductor terminals expose caused by the insulating layer retraction after the temperature alternations, the electrical short-circuit risk exists. An Verification method of cable insulation retraction experienced high and low temperature alternations based on allometric growth model is proposed in this paper, the Verification model fitted curve of the contraction amounts along the wire axis of the wire insulating layer is built through ground test data, which is used to predict the contraction amount of the insulating layer at the wire terminal after experienced extreme temperature alternations many times and assess the insulation protection of conductor terminals inside electrical connectors at both ends of a cable. The Verification method provides a reference to the reliability and security design of cables under extreme temperature environment in deep space exploration.

     

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