[1] ZHANG K, CHOU S, ANG S, et al.A MEMS-based solid propellant microthruster with Au/Ti igniter [J].Sensors and Actuators A:
Physical,2005,122(1):113-123.
[2] BRIAND D, PHAM P, ROOIJ N.Reliability of freestanding polysilicon microheaters to be used as igniters in solid propellant
microthrusters [J].Sensors and Actuators A: Physical,2007,135(2):329-336.
[3] TANAKA S, KONDO K, HABU H, et al.Test of B/Ti multilayer reactive igniters for a micro solid rocket array thruster[J]. Sensors and
Actuators A: Physical,2008,144(2):361-366.
[4] ROSSI C, ORIEUX S, LARANGOT B, et al. Fabrication and modeling of solid propellant microrocket-application to micropropulsion [J].
Sensors and Actuators A: Physical,2002,99 (1/2):125133.
[5] LINDSAY W, TEASDALE D, MILANOVIC V, et al. Thrust and electrical power from solid propellant microrockets. 2. Actuators\[C\]∥ Micro
Electro Mechanical Systems, 2001. MEMS 2001. The 14th IEEE International Conference on. Interlaken.Switzerland: IEEE, 2001: 606610.
[6] ZHANG K, CHOU S, ANG S. Investigation on the ignition of a MEMS solid propellant microthruster before propellant combustion[J].
Journal of Micromechanics and Microengineering, 2007, 17(2):322.
[7] 刘建, 沈瑞琪,叶迎华,等.微细圆管中B/KNO3燃烧特性分析[J].含能材料,2010,18(3):335338.
LIU Jian,SHEN Rui-qi,YE Ying-hua,et al.Combustion characteristics of B/KNO3 in microscale tube [J].Chinese Journal of Energetic
Materials,2010,18(3):335338.
[8] 董磊,康小明,孙小兵,等.内壁经微弧氧化处理的微型固体火箭温度场的数值模拟[J].固体火箭技术,2009,32(6):625637.
DONG Lei,KANG Xiao-ming,SUN Xiao-bing, et al.Numerical simulation of temperature fields of solid propellant micro-rocket with inner wall
treated by PMAO techniques [J].Journal of Solid Rocket Technology, 2009, 32(6):625637.
[9] 徐超.MEMS固体微推进器的设计与制备\[D\].长沙:国防科学技术大学,2006.
XU Chao. Design and fabrication of MEMS based solid propellant micro thruster \[D\]. Changsha: National University of Defense Technology,
2006.
[10] 陈旭鹏,李勇,周兆英.微小型化学能推进器的研究[J].微纳电子技术,2003, (7/8):456460.
CHEN Xu-peng,LI Yong,ZHOU Zhao-ying.Research into micro chemical thrusters[J].Micronanoelectronic Technology,2003, (7/8):456460.
[11] 马立志,沈瑞琪,叶迎华.不同装药条件下的微化学推冲器的推进性能研究[J].兵工学报,2004,25(5):547550.
MA Li-zhi,SHEN Rui-qi,YE Ying-hua. A study on the thruster properties of micro chemical thrusters charged with different propellants
[J].Acta Armanmentarii,2004,25(5):547550.
[12] 尤政,张高飞,任大海.MEMS微推进技术的研究[J].纳米技术与精密工程,2004,2(2):98105.
YOU Zheng,ZHANG Gao-fei,REN Da-hai.Study on MEMS micro-thruster technology[J]. Nanotechnology and Precision Engineering,2004, 2(2) :98105.
[13] LARANGOT B, ROSSI C, CAMPS T, et al. Solid propellant micro-rockets-towards anew type of power mems [J]. Nanotech, 2002:912.
[14] CHAALANE A, ROSSI C, ESTEVE D. The formulation and testing of new solid propellant mixture(DB+x%BP) for a new MEMS-based microthruster
[J]. Sensors and Actuators A: Physical, 2007, 138(1):161166.
[15] CAROLE R, BENOIT L, DENIS L, et al. Final characterizations of MEMS-based pyrotechnical microthrusters [J]. Sensors and Actuators A:
Physical, 2005, 121(2):508514.
[16] RUDNYI E B, BECHTOLD T, KORVINK J G, et al. Solid propellant microthruster: Theory of operation and modelling strategy\[C\]∥ NanoTech
2002-“At the Edge of Revolution”. Houston, Texas: AIAA paper, 2002: 19.
[17] CHOU S, YANG W, CHUA K, et al. Development of micro power generators A review [J]. Applied Energy, 2001, 88(1):116.
[18] JU Y, MARUTA K. Microscale combustion: technology development and fundamental research [J]. Progress in Energy and Combustion
Science, 2011, 37(6):669715.
[19] MARUTA K. Micro and mesoscale combustion [J]. Progress in Energy and Combustion Science, 2011, 33(1):125150.
[20] 毛成立,李葆萱,胡松启,等.热空气中硼粒子点火模型研究综述[J].推进技术,2001,22(1):69.
MAO Cheng-li,LI Bao-xuan,HU Song-qi,et al.Overview of models of boron particle ignition in hot air [J].Journal of Propulsion
Technology,2001, 22(1):69.
[21] CHEN D, HSIEH W, SNYDER T, et al. Combustion behavior and thermophysical properties of metal-based solid fuels [J]. Journal of
Propulsion and Power, 1991, 7(2): 250257.
[22] 林振坤,韩咚林,王天放,等.空气条件下氧化剂对铝/水基燃料燃烧特性的影响[J].含能材料,2010,18(3):295299.
LIN Zhen-kun,HAN Dong-lin,WANG Tian-fang, et al. Effects of oxidants on combustion performances of Al/H2O based fuels in air [J]. Chinese
Journal of Energetic Materials,2010,18(3) : 295299.
[23] SPALDING M J, KRIER H, BURTON R L. Emission spectroscopy during ignition of boron particles at high pressure\[C\]∥ 35th Aerospace
Sciences Meeting and Exhibit. Reno, NV: AIAA Paper, 1997: 116. |