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FY-2C星热设计的优化及其在轨性能 被引量:2

Optimization of Thermal Control Design for FY-2C Meteorological Satellite and Its On-Orbit Performance
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摘要 为改善风云二号(FY-2)C气象卫星有效载荷扫描辐射计及其他星上仪器的热环境温度,采用前太阳屏增加散热面、二次分离环提高散热能力,以及重组与补充热控电加热器方案对其热控分系统进行了优化,并用仿真分析和局部试验替代了热平衡试验验证。C星飞行结果表明,优化后的热控分系统具有良好的调控和适应能力,工作稳定,性能指标全部满足要求。说明C星的热设计优化正确有效,为扫描辐射计光机提供了优良的热环境温度。 To improve the thermal environment of seanning radiometer for FY-2C meteorological satellite, the measures such as increasing radiator of solar screen, heightening heat dissemination of second separation ring, and reorganizing and supplying electric heater were taken to optimize the thermal control subsystem in this paper. The simulation analysis and partial test were used to replace thermal balance approval. The flying result of FY-2C satellite showed that the optimized thermal control subsystem had a good ability of control, adjustment and adapting, which operated stably. The performance satisfied the requirements, All these proved that the thermal design optimization of FY-2C satellite was correct and effective, and provided the sensor of scanning radiometer a good thermal environment.
出处 《上海航天》 北大核心 2005年第B12期55-60,共6页 Aerospace Shanghai
关键词 风云二号气象卫星 热设计 环境温度 优化 验证 性能 FY-2 meteorological satellite Thermal design Environment temperature Optimization Approval Performance
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  • 1刘伟,杨沪宁.“天绘一号”卫星热控设计及飞行验证[J].遥感学报,2012,16(S1):61-65. 被引量:2
  • 2周佐新,华诚生.SR107-ZK白漆在轨飞行性能退化分析[J].航天器工程,2007,16(3):78-81. 被引量:5
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  • 8侯增祺;胡金刚.航天器热控制技术--原理及其应用[M]{H}北京:中国科学技术出版社,2007.
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