期刊文献+

MEMS固体微推进器中Cr薄膜点火电阻的研究 被引量:22

Research on the Cr Membrane Igniting Resistance in MEMS Solid Propellant Micro-Thruster
下载PDF
导出
摘要 点火电路是MEMS固体化学微推进器中最重要的组成部分,其点火电压的大小及点火可靠性则主要取决于点火电阻.国内外均采用多晶硅(polysilicon)或贵金属铂(Pt)作为点火电阻材料,所制备出来的点火电阻的阻值都比较大,需要的点火电压较高(40V以上),而且点火可靠性不高,难以满足固体微推进器的使用要求.本文首次采用金属铬(Cr)作为点火电阻材料,设计了具有高可靠性的并联点火电阻图形,通过磁控溅射镀膜、光刻以及Cr的湿法腐蚀工艺制备出了Cr薄膜点火电阻,并在20伏左右的低电压下成功地实现了常规火药黑索金的点火,为低点火电压、低成本、高可靠性的点火电路的制备提供了一条有效的技术途径. Igniter is the most important part of MEMS solid propellant micro-thruster, and its igrating voltage and igniting reliability are mainly decided by the igniting resistance. Polysilicon and Pt are the two main materials for the igniting resistance. As the resistance is usually very high, the igniters need higher voltage (over 40 voltages) to work, and their igniting reliabilities are not high enough, which can't meet the requirements of the micro-thruster. Cr is chosen as the igniting resistance material for the first time, and a new highly reliable parallel connection resistance shape is designed. The Cr membrane igniting resistance is fabricated by the process of magnetron-sputtering, lithography, and wet etching, and it can successfully ignite the common powder RDX at the low voltage of 20 voltages, which provides an effective way of fabrication of the igniters which have lower igniting voltage, lower cost and higher igniting reliabilities.
出处 《传感技术学报》 CAS CSCD 北大核心 2006年第05A期1411-1414,1418,共5页 Chinese Journal of Sensors and Actuators
关键词 MEMS 微推进器 点火电阻 铬薄膜 点火电压 MEMS micro-thruster igniting resistance Cr membrane igniting voltage
  • 相关文献

参考文献10

  • 1Groot W A. Propulsion Options for Primary Thrust and Attitude Control of Mierospaeeeraft[R]. NASA Technical Report,Brook Park, Ohio, USA, March 1998, NASA/CR-1998-206608. 被引量:1
  • 2尤政,张高飞.基于MEMS的微推进系统的研究现状与展望[J].微细加工技术,2004(1):1-8. 被引量:18
  • 3Zhang K L, Chou S K, Ang S S. MEMS-Based Solid Propellant Microthruster Design, Simulation, Fabrication, and Testing[J]. Journal of MicroElectroMechanical Systems, 2004,13(2): 165 - 175. 被引量:1
  • 4Larangot B, Conedera V, Dubreuil P, et al. Solid Propellant MicroThruster : an alternative propulsion device for nanosatellite[C] // Aerospace Energetic Equipment Conference, Avignon, France, 2002. 被引量:1
  • 5Youngner D W, Lu S T, Choueiri E, et al. MEMS Mega-pixel Micro-thruster Arrays for Small Satellite Stationkeeping[C]///14th Annual/USU Conference on Small Satellites, 2000,SSCO0-X-2. 被引量:1
  • 6Lewis D H, Jr. , Janson S W, et al. Digital Miero Propulsion[C]//12th IEEE International Micro Electro Mechanical Systems Conference, January 17-21, 1999. 被引量:1
  • 7Larangot B, Rossi C, Camps T, et al. Solid Propellant Microrockets-Towards A New Type of Power MEMS[C]// Nanotech AIAA 2002-5758, Houston, September 9-12, 2002. 被引量:1
  • 8Lee J K, Lee D H, Kwon S. Design and Performance Evaluation of Components of Micro Solid Propellant Thruster[C]//40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Fort Lauderdale, Florida, July 11-14, 2004. 被引量:1
  • 9张高飞,尤政,胡松启,李葆萱,王伯雄.基于MEMS的固体推进器阵列[J].清华大学学报(自然科学版),2004,44(11):1489-1492. 被引量:25
  • 10许并社..纳米材料及应用技术[M],2004.

二级参考文献16

  • 1Ye X Y, Tang F, Ding H Q, et al. Study of a vaporizing water micro-thruster[ J ]. Sensors and Actuators A:Physical,2001,89( 1 -2) :159 - 165. 被引量:1
  • 2Maurice Martin,Howard Schlossberg,Joe Mitola, et al. University nanosatellite program[A]. IAF Symposium[C]. Redondo Beach(USA) :IAF,1999. 被引量:1
  • 3Pranajaya F,Cappelli M. Progress on Colloid Micro-thruster Research and Flight Testing[R]. USA:Stanford University,2000. 被引量:1
  • 4David H,Siegfried W, Ronald B,et al. Digital micropropulsion[J]. Sensors and Actuators A:Physical,2000,80(2) :143 - 154. 被引量:1
  • 5Daniel W Youngner,Son Thai Lu,Edgar Choueiri,et al. MEMS mega-pixel micro-thruster arrays for small satellite station keeping[ A]. 14thAnnual/USU Conference on Small Satellites[ C]. Logan(USA) :AIAA,2000. 被引量:1
  • 6Rachel Leach,Kerry L Neal. Discussion of micro-Newton thruster requirements for a drag-free control system[ A]. 16th Annual/USU Conference on Small Satellites[ C]. Logan(USA) :AIAA,2002. 被引量:1
  • 7Fleeter R. Microspacecraft [ M ]. Reston(USA) :The Edge City Press, 1995. 被引量:1
  • 8Juergen Muller, Colleen Marrese,James Polk, et al. An overview of MEMS-based micropropulsion developments at JPL[ J]. Acta Astronautics,2003,52(9 - 12) :881 - 895. 被引量:1
  • 9Dana Teasdale. Solid Propellant Microrockets[ D]. Berkeley:University of California,2000. 被引量:1
  • 10Fleeter R. Microspacecraft [M]. Reston, VA: The Edge City Press, 1995. 被引量:1

共引文献39

同被引文献119

引证文献22

二级引证文献76

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