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金星气球环境分析与热动力研究

雷岩鹏 杨春信

雷岩鹏, 杨春信. 金星气球环境分析与热动力研究[J]. 航空动力学报, 2012, 27(11): 2505-2510.
引用本文: 雷岩鹏, 杨春信. 金星气球环境分析与热动力研究[J]. 航空动力学报, 2012, 27(11): 2505-2510.
LEI Yan-peng, YANG Chun-xin. Study of environment analysis and thermodynamic on Venus balloon[J]. Journal of Aerospace Power, 2012, 27(11): 2505-2510.
Citation: LEI Yan-peng, YANG Chun-xin. Study of environment analysis and thermodynamic on Venus balloon[J]. Journal of Aerospace Power, 2012, 27(11): 2505-2510.

金星气球环境分析与热动力研究

Study of environment analysis and thermodynamic on Venus balloon

  • 摘要: 分析了金星独特的大气环境,归纳了影响金星气球飞行的主要环境因素,并建立了数学模型.依据金星气球的投放、飘浮程序,设计了金星原型氦气球,设计驻留高度为35km.建立了金星气球热动力仿真平台.计算结果表明:金星气球在30~40km高度释放,可快速到达驻留高度并作长期飘浮;金星气球系统的温度范围为440~520K,最大速度低于10m/s.这为进一步开展对金星气球的研究提供了依据.

     

  • [1] Landis G.Low altitude exploration of the Venus atmosphere by balloon [R].AIAA-2010-628777,2010.
    [2] Sagdeev R Z.An overview of the Soviet vega balloon experiment and studies of the atmosphere of Venus [R].Washington,D.C.:NASA center for aerospace information (CASI),1986.
    [3] Van den Berg M L,Falkner P,Atzei A C,et al.Venus entry probe technology reference study[J].Advances in Space Research,2006,8(11):2626-2632.
    [4] Titov D V,Svedhem H,Koschny D,et al.Venus express science planning[J].Planetary and Space Science,2006,54(13/14):1279-1297.
    [5] Hall J L,Kerzhanovich V V,Yavrouian A H,et al.Second generation prototype design and testing for a high altitude Venus balloon[J].Advances in Space Research,2009,44(1):93-105.
    [6] Hall J L,Fairbrother D,Kerzhanovich V V,et al.Prototype design and testing of a Venus long duration,high altitude balloon[J].Advances in Space Research,2008,42(10):1648-1655.
    [7] 马云鹏,武哲,吕明云,等.高空气球综合/开放式设计系统[J].北京航空航天大学学报,2010,36(1):61-64. MA Yunpeng,WU Zhe,LV Mingyun,et al.High-altitude balloon integration/opening design system[J].Journal of Beijing University of Aeronautics and Astronautics,2010,36(1):61-64.(in Chinese)
    [8] 姚伟,李勇,王文隽,等.平流层飞艇热力学模型和上升过程仿真分析[J].宇航学报,2007,28(3):603-607. YAO Wei,LI Yong,WANG Wenjun,et al.Thermodynamic model and numerical simulation of a stratospheric sirship take-off process[J].Journal of Astronautics,2007,28(3):603-607.(in Chinese)
    [9] 方贤德,王伟志,李小建.平流层飞艇热仿真初步探讨[J].航天返回与遥感,2007,28(2):5-9. FANG Xiande,WANG Weizhi,LI Xiaojian.A study of thermal simulation of stratospheric airships[J].Spacecraft Recovery & Remote Sensing,2007,28(2):5-9.(in Chinese)
    [10] Bachelder K N M H,Hall J,Jones J,et al.Venus geoscience aerobot study (VEGAS) [R].AIAA-99-3856,1999.
    [11] 丁国良.制冷空调新工质:热物理性质的计算方法与实用图表[M].上海:上海交通大学出版社,2003.
    [12] Carlson L A,Horn W J.New thermal and trajectory model for high-altitude balloons[J].Journal of Aircraft,1983,20(6):500-507.
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出版历程
  • 收稿日期:  2011-11-24
  • 刊出日期:  2012-11-28

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