期刊文献+

多残渣富燃料推进剂燃速测试仪的改进 被引量:5

Improving on burning rate testing apparatus of fuel-rich propellants
下载PDF
导出
摘要 在现有靶线法燃速测试仪的接线柱上加装绝缘防烧蚀挡板,解决了燃烧过程中的非正常中断问题。设计并安装过滤除尘器,解决了残渣污染气体管路的问题。在燃烧室上连接压强传感器,实现了燃烧过程中压强变化的监测。实验结果表明,改进后的靶线法燃速测试仪推进剂药条燃烧过程准确,实验后清理简便可靠,且保障了管路的密封,实现了多残渣富燃料推进剂燃速的正确测试。 Iadditional installation of an insulating anti-erosion tailgate upon the posts present the strand-burner-method burning rate testing apparatus is a solution to irregular interruption in the process of combustion.A filter designed and fixed is capable of avoiding pollution of the residues.Connecting a pressure sensor with the combustion chamber makes it possible to keep accurate records of pressure.The experimental results show that the strand-burner-method burning rate testing apparatus that has been improved mentioned above is accurate in the combustion process of propellant strands,simple and reliable in the cleaning-up after the experiment,secure in the sealing of the pipeline,and successful in the burning rate test of multi-residue fuel-rich propellants.
出处 《固体火箭技术》 EI CAS CSCD 北大核心 2010年第3期360-362,共3页 Journal of Solid Rocket Technology
关键词 富燃料推进剂 残渣 燃速测试 靶线法 fuel-rich propellants residue buring rate testing strand burner method
  • 相关文献

参考文献4

二级参考文献15

  • 1毛成立,李葆萱.贫氧推进剂一次燃烧产物的热力计算[J].宇航学报,2000,21(z1):32-37. 被引量:6
  • 2Frederick R J,Traineau J C,Marthe Popo.Review of ultrasonic technique for steady state burning rate measurements[C]∥ 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.Washington,DC:American Institute of Aeronautics and Astr-onautics,2000.
  • 3Salvo R D,Frederick R A J.Direct ultrasonic mea-surement of solid propellant ballistics[C]∥ 35th AIAA/ASME/SAE/ASEE Joint Propulsion Confe-rence & Exhibit.Washington DC:American Institute of Aeronautics and Astronautics,1999.
  • 4Dauch F,Moser M D,Frederick R A,et al.Unc-ertainty assessment of ultrasonic measurement of propellant burning rate[C]∥ 35th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.Washington DC:American Institute of Aeronautics and Astronautics,1999.
  • 5Cauty F,Demarais J C.Ultrasonic me-asurements of the uncured solid propellants burning rate[C]∥ Proceedings of the 21th International Congress of ICT.Karlsruhe:ICT,1990.
  • 6Thomas J H,Jeffrey J M,Hermen k.Ultrasonic me-asurements of the pressure-coupled response function at low frequency for composite solid propellants[C]∥ 38th AIAA/ASME/SAE/ASEE Joint Propulsion Con-ference & Exhibit.Washington DC:American Ins-titute of Aeronautics and Astronautics,2002.
  • 7Murphy J J,Chai S,Brdar C R,et al.Function me-asurement using an ultrasonic technique in an oscillatory burner[C]∥ 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.Washington DC:American Institute of Aeronautics and Astronautics,2000.
  • 8Salvo R Di,Frederick R A Jr.Direct ultrasonic mea-surement of solid propellant combustion transients[C]∥ 35th AIAA/ASME/SAE/ASEE Joint Pr-opulsion Conference & Exhibit.Washington DC:American Institute of Aeronautics and Astronautics,1999.
  • 9Murphy J J,Martin A O,Krier H.Precision techn-ique for measuring burning rates of solid propellants during pressure transients[C]∥ 36thAerospace Science Meeting & Exhibit.Washington DC:Ame-rican Institute of Aeronautics and Astronautics,1998.
  • 10Traineau J C,Kuentzmann P.Some measurements of solid propellant burning rates in nozzleless motors[C]∥20thAIAA/ASME/SAE Joint Propulsion Con-ference.Washington DC:American Institute of Aer-onautics and Astronautics,1984.

共引文献11

同被引文献86

引证文献5

二级引证文献21

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