留言板

尊敬的读者、作者、审稿人, 关于本刊的投稿、审稿、编辑和出版的任何问题, 您可以本页添加留言。我们将尽快给您答复。谢谢您的支持!

姓名
邮箱
手机号码
标题
留言内容
验证码

羽流效应地面模拟试验系统关键技术发展

王文龙 周建平 蔡国飙

王文龙, 周建平, 蔡国飙. 羽流效应地面模拟试验系统关键技术发展[J]. 航空动力学报, 2012, 27(4): 900-906.
引用本文: 王文龙, 周建平, 蔡国飙. 羽流效应地面模拟试验系统关键技术发展[J]. 航空动力学报, 2012, 27(4): 900-906.
WANFG Wen-long, ZHOU Jian-ping, CAI Guo-biao. Development of vacuum plume effects ground simulation experimental system key technology[J]. Journal of Aerospace Power, 2012, 27(4): 900-906.
Citation: WANFG Wen-long, ZHOU Jian-ping, CAI Guo-biao. Development of vacuum plume effects ground simulation experimental system key technology[J]. Journal of Aerospace Power, 2012, 27(4): 900-906.

羽流效应地面模拟试验系统关键技术发展

基金项目: 中俄航天合作项目

Development of vacuum plume effects ground simulation experimental system key technology

  • 摘要: 叙述了羽流效应地面模拟试验系统由高空模拟试车台向真空试验系统发展的过程,指出引射原理的局限性和低温冷凝技术的适用性.介绍了应用低温冷凝技术建成的美国CHAFF-4(the collaborative high altitude flow facility-Ⅳ)系统和德国STG(Simulationsanlage für Treibstrahlenin Göttingen)系统及中国首座大型羽流效应地面模拟试验系统——PES(the plume effects experimental system)系统.采用直接模拟蒙特卡罗DSMC (direct simulation Monte Carlo )方法对PES设备的内置式液氦深冷泵的抽气能力进行了数值模拟研究,结果表明无论有无羽流吸附泵时,2g/s级发动机点火时,内置式液氦深冷泵都能满足发动机出口截面后 ø 4m×5m范围内的背压小于10-3 Pa,羽流吸附泵能有效地阻止压缩波向喷管方向推进.

     

  • [1] 蔡国飙,祖国君,王慧玉,等.羽流问题研究概况[J].推进技术,1995,16(4):50-54. CAI Guobiao,ZU Guojun,WANG Huiyu,et al.The sketchy situation of study on plume[J].Journal of Propulsion Technoogy,1995,16(4):50-54.(in Chinese)
    [2] 黄本诚.空间模拟器设计[M].北京:宇航出版社,1994.
    [3] 黄本诚,马有礼.航天器空间环境试验技术[M].北京:国防工业出版社,2002.
    [4] 黄本诚,童靖宇.空间环境工程学[M].北京:中国科学技术出版社,2010.
    [5] 达道安.真空设计手册 [M].3版.北京:国防工业出版社,2006.
    [6] 李殿东.76km高空环境模拟试验舱的研制[J].真空,2002,39(5):41-45. LI Diandong.Design of 76km high-altitude space simulation test module[J].Vacuum,2002,39(5):41-45.(in Chinese)
    [7] 黄本诚.KM6载人航天器空间环境试验设备[J].中国空间科学与技术,2002,22(3):1-6. HUANG Bencheng.Space environment test facility for manned spacecraft[J].Chinese Space Science and Technology,2002,22(3):1-6.(in Chinese)
    [8] 陈金明,黄本诚,袁修干,等.载人试验舱的结构设计及有限元分析[J].中国空间科学与技术,2002,22(3):13-19. CHEN Jinming,HUANG Bencheng,YUAN Xiugan,et al.Structure design and finite element calculation of km6 manned test chamber[J].Chinese Space Science and Technology,2002,22(3):13-19.(in Chinese)
    [9] Piesik E T,Koppang R R,Simkin D J.Rocket exhaust impingement on a flat plate at high vacuum[J].J.Spacecraft Rockets,1966,3(11):1650-1657.
    [10] Andrew D K.An overview of ground based spacecraft-thruster interaction studies:facility design issues.AIAA-2000-0463,2000.
    [11] Lutfy F M,Vargo S E,Muntz E P,et al.Weaver collaborative high altitude flowf acility’s CHAFF-4 for studies of spacecraft propulsion plumes and contamination.AIAA 98-3654,1998.
    [12] Dettleff G,Klaus P.Initial experimental results from the new DLR-high vacuum plume test facility STG.AIAA 93-3297,1997.
    [13] Georg D Klaus P.Initial experimental results from the new DLR-High vacuum plume test facility STG.AIAA 97-3297,1997.
    [14] Georg D,Klaus P.Experimental investigation of fully expanding free jets and plumes //Proceedings of 21st International Symp.Rarefied Gas Dynamics.Toulouse:American Institute of Physics,1999:607-614.
    [15] Plhn K,Dettleff G.Modelling of N2-thruster plumes based on experiments in STG //Proceedings of the 22nd Symposium on Rarefied Gas Dynamics.Sydney :American Institute of Physics,2000:848-855.
    [16] Georg D.Heat transfer measurements on a plate adjacent to a bipropellant thruster //Proceedings of 3rd International Conference on Spacecraft Propulsion.Cannes:European Space Agency,2000:627-634.
    [17] Lutfy F M,Vargo S E,Muntz E P,et al.Weaver collaborative high altitude flow facility’s CHAFF-4 for studies of spacecraft propulsion plumes and contamination. AIAA 98-3654,1998.
    [18] Ketsdever A D,Jamison A E,Muntz E P,et al.An advanced cryogenic pumping concept for spacecraft-thruster interaction and contamination facilities.AIAA 2000-2362,2000.
    [19] Lutfy F M,Green A A,Muntz E P,et al.Investigation of the operational envelope of the CHAFF-Ⅳ plume and contamination thermospheric flow simulator.AIAA 99-2719,1999.
    [20] Muntz E P.Significant increase in the cryogenic pumping system capacity and reliability for the CHAFF-Ⅳ plume and contamination facility.ADA412533,2002.
    [21] Ketsdever A D,Young M P,Jamison A,et al.Investigation of the unique cryogenic pumping system of the CHAFF-Ⅳ spacecraft-thruster interaction facility.ADA40 9037, 2001.
    [22] Lutfy F M,Muntz E P,Ketsdever A D.Investigation of the operational envelope of the CHAFF-4 plume and contaminationfacility.ADA408796,1999.
    [23] Muntz E P,Lutfy F,Ketsdever A,et al.Collaborative high altitude flow facility (CHAFF):university facility for studies of high altitude propulsion plumes,liquids and gas releases,and interactions;final technical rept..ADA367070,1999.
  • 加载中
计量
  • 文章访问数:  1708
  • HTML浏览量:  140
  • PDF量:  539
  • 被引次数: 0
出版历程
  • 收稿日期:  2011-05-09
  • 修回日期:  2011-08-14
  • 刊出日期:  2012-04-28

目录

    /

    返回文章
    返回