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双组元统一推进系统优化改进技术进展 被引量:4

Progress of optimization for bipropellant uniform propulsion system
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摘要 不断提高推进剂在轨管理效率,是应用卫星对推进系统的基本要求,也是推进系统的重要发展方向。推进剂剩余量在轨高精度测量和并联贮箱均衡排放主动控制,是提高推进剂在轨管理效率的重要技术手段。针对我国SAST-5000卫星平台双组元统一推进系统,开展了气体注入压力激励方法的关键技术攻关,并取得重要进展。研究结果表明:改良型气体注入压力激励法的推进剂剩余量在轨测量精度达到-0.68%-0.66%,并联贮箱均衡排放控制措施将被动调节的不均衡度控制在优于1.13%,主动纠偏措施还可进一步提高并联贮箱排放推进剂的同步性。 Application satellites have a great demand on improving the efficiency ot on-boara management of propellant, which is also the demand of propulsion system development. The high-accuracy on-board gauging of the propellant remaining quantity and equalizing expulsion active control of parallel tanks are the important technological means for improving the on-board management efficiency of propellant. The propellant gauging technology using gas injecting method and the technology for equalizing expulsion of parallel propellant tanks were investigated for Chinese SAST-5000 satellite platform. The research result shows that the on-board gauging precision of gas injecting method is -0.68% to 0.66%, and the equalizing expulsion of parallel propellant tanks is 1.13%. The active correction measures can also improve the synchronization of propellant expulsion of parallel tanks.
出处 《火箭推进》 CAS 2014年第6期8-12,共5页 Journal of Rocket Propulsion
基金 中国航天科技集团公司支撑项目(2009JY02)
关键词 双组元 统一推进系统 剩余推进剂测量 均衡排放 bipropellant uniform propulsion system remaining propellant gauging equalizing expulsion
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  • 1张冬辰.军事通信[M].北京:国防工业出版社,2008.
  • 2Maral G,Bousquet M.Satellite Communication System,Techniques and Technology.4th ed[M].New York:John Wiley Sons,Ltd.,2002.
  • 3Cebrowski A K,Garstka J J.Network-Centric Warfare:Its Origin and Future[R].U.S:Jan,1998.
  • 4Maurics M,McKinney M.Transformational Satellite (TSAT) Communication System[R].Ala:USAF Air University,2007.
  • 5Space Communications Plan 2007[R].Washington,DC:National Aeronautics and Space Administration,2007.
  • 6贝尔 H D,工程热力学理论基础及工程应用,1983年
  • 7杨宝贵,液体推进剂处理、贮存和运输(译),1976年
  • 8匿名著者,深冷手册,1973年
  • 9Chang Y K,AIAA94-2512
  • 10郭霄峰.液体火箭发动机试验[M].北京:宇航出版社,1990.

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