期刊文献+

常规推进剂在轨加注技术研究现状与趋势 被引量:6

Current Situation and Trend Analysis on Orbital Refueling Technology for Storable Propellants
在线阅读 下载PDF
导出
摘要 实现推进剂的在轨加注服务能够显著提升大规模空间探测能力、减小运载器规模、降低任务成本。归纳常规推进剂在轨加注方案并进行分类和比较,对国外典型的常规推进剂在轨加注研究计划进行分析,总结其发展趋势,为后续深入开展相关研究工作提供参考。 The realization of orbital refueling service for spacecraft can significantly improve the ability of large scale exploration missions, reduce the takeoff weight and dimension of the launch vehicles and aerospace vehicles, and reduce the exploration cost. In this paper, orbital refueling schemes for storable propellants are induced, classified and compared. The representative orbital refueling research programs of USA are analyzed, and the development trends are summed up, which provides reference for future in-depth research.
出处 《导弹与航天运载技术》 北大核心 2015年第5期50-54,共5页 Missiles and Space Vehicles
关键词 在轨加注 常规推进剂 研究进展 On orbital refueling Storable propellant Research trend
  • 相关文献

参考文献14

  • 1Eberhardt R, Tracey T, Bailey W. Orbital spacecraft technology[C]. Huntsville: AIAA/ASME/SAE/ASEE, Joint resupply PropulsionConference, 1986.
  • 2Clark P. The soviet manned space program[M]. Phoenix: Orion Press, 1988.
  • 3Chato D J. Experimentation for the maturation of deep space cryogenic refueling technologies[R]. NASA/TP-2008-214929, 2008.
  • 4Lacovic R. Propellant management report for the titan/centaur TC-5 extended mission[R]. NASA-TM-73749. 1977.
  • 5Chato D J, Martin T A. Vented tank resupply experiment-flight test results[R]. NASA-TM- 107498, 1997.
  • 6Tegart J, Kirkland Z. On-orbit propellant resupply demonstration-flight test results[C]. Monterey: AIAA/SAE/ASME/ASEE, 21st Joint Propulsion Conference, 1985.
  • 7Dominick S, Driscoll S. Fluid acquisition and resupply experiment (Fare I) flight results[C]. Monterey: AIAA/SAE/ASME/ASEE, 29th Joint Propulsion Conference& Exhibit, 1993.
  • 8Michael D B. Tank pressure control experiment-results of three space flights[C]. Seattle: AIAA/ASME/SAE/ASEE, 33rd Joint Propulsion Conference&Exhibit, 1997.
  • 9Rotenberger S, SooHoo D, Abraham G. Orbital express fluid transfer demonstration system[C]. Sensors and Systems for Space Applications II, 2008.
  • 10Robert B. Orbital express program summary and mission overview[C]. Sensors and Systems for space applications II, 2008.

二级参考文献8

  • 1Lacovic R. Propellant management report for the titan/ centaur TC-5 extended mission[ R ]. NASA-TM-73749, 1977.
  • 2Chato D J, Martin T A. Vented tank resupply experi- ment--flight test results[ R ]. NASA- TM-107498,1997.
  • 3Michael D B. Tank pressure control in low gravity by jet mixing[R]. NASA-CR-191012, 1993.
  • 4Kirkland Z, Tegart J. On-orbit propellant resupply dem- onstration [ C ]. AIAA/SAE/ ASME, 20th Joint Propul- sion Conference, ohio,USA, Junel 1-13 , 1984.
  • 5Tegart J, Kirkland Z. On-orbit propellant resupply dem- onstration - flight test results[ J]. AIAA/SAE/ASME/ ASEE, 21st Joint Propulsion Conference, Monterey, CA, July 8-10, 1985.
  • 6Dominick S, Driscoll S. Fluid acquisition and resupply experiment ( Fare I) flight results [ J ]. AIAA/SAE/ ASME/ASEE, 29th Joint Propulsion Conference & Exib- it, Monterey, CA, June 28-30, 1993.
  • 7Michael D B. Tank pressure control experiment - results of three space flights [ J ]. AIAA/ASME/SAE/ASEE, 33ra Joint Propulsion Conference & Exhibit, Seattle, WA, July 6-9, 1997.
  • 8胡齐,李永,耿永兵,陈健.一种板式推进剂管理装置(PMD)性能的数值仿真[J].空间控制技术与应用,2010,36(3):55-58. 被引量:6

共引文献7

同被引文献73

引证文献6

二级引证文献5

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部