一种双组元推进系统极性测试方法及应用
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摘要
针对航天器推进系统极性测试方法不完善的问题,通过对推进系统极性测试需求的分析,提出了推进系统极性测试确认方法,进而设计了一种双组元推进极性测试系统,并通过地面工艺试验,确定了测试关键参数及采集工装的有效性。该方法已成功应用于航天器测试任务,充分验证了推进极性测试方法及测试系统的正确性、有效性。
The method of polarity test for spacecraft propulsion system is not perfect.By analyzing the requirement of propulsion system polarity test,this paper proposes a method of propulsion system polarity test confirmation,and then designs a bipropellant propulsion polarity test system.Through ground process test,the test key parameters and the validity of the acquisition tool are confirmed.The method has been successfully applied to the spacecraft test task,which fully verified the correctness and effectiveness of the propulsion polarity test method and test system.
The method of polarity test for spacecraft propulsion system is not perfect.By analyzing the requirement of propulsion system polarity test,this paper proposes a method of propulsion system polarity test confirmation,and then designs a bipropellant propulsion polarity test system.Through ground process test,the test key parameters and the validity of the acquisition tool are confirmed.The method has been successfully applied to the spacecraft test task,which fully verified the correctness and effectiveness of the propulsion polarity test method and test system.
引文
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[2]于登云.月球软着陆探测器技术[M].北京:国防工业出版社,2016Yu Dengyun.Lunar soft landing probe technology[M].Beijing:National Defence Industry Press,2016(in Chinese)
[3]谭维炽,胡金刚.航天器系统工程[M].北京:中国科学技术出版社,2009Tan Weichi,Hu Jingang.Spacecraft system engineering[M].Beijing:China Science and Technology Press,2009(in Chinese)
[4]屠善澄.卫星姿态动力学与控制[M].北京:中国宇航出版社,2009Tu Shancheng.Satellite attitude dynamic and control[M].Beijing:China Astronautics Press,2009(in Chinese)
[5]毛根旺,唐金兰.航天器推进系统及其应用[M].西安:西北工业大学出版社,2009Mao Genwang,Tang Jinlan.Spacecraft propulsion system and its applications[M].Xi’an:Northwestern Polytechnical University Press,2009(in Chinese)
[6]中国航天工业总公司航天工业行业标准.QJ 2730-95弹道式导弹和运载火箭控制系统极性规定[S].北京:航天标准化研究所,1995Industry Standard of China Aerospace Industry Corporation.QJ 2730-95polarity regulations for control systems of missile-guided missiles and launch vehicles[S].Beijing:Institute of Space Standardization,1995(in Chinese)
[7]M A Schwende,G Munding,G Schute.Bipropellant thruster family for spacecraft propulsion[C]//TN Joint Propulsion Conference and Exhibit.Washington D.C.AIAA,1992
[8]谢红军,洪鑫.深空探测器推进系统[J].上海航天,2003,20(2):38-43Xie Hongjun,Hong Xin.Deep space probe propulsion system[J].Shanghai Aerospace,2003,20(2):38-43(in Chinese)
[9]韩泉东.国外深空探测推进技术发展及启示[J].火箭推进,2017Han Quandong.Development of propulsion technology abroad for deep space exploration and its inspiration[J].Journal of Rocket Propulsion,2017(in Chinese)