线性喷管构形对激光推力器冲量耦合系数的影响
[1] Kantrowitz A.Propulsion to orbit by ground-based laser[J].Astronautics and Aeronautics,1972,10(5):74.
[2] Schall W O,Bohn W L,Eckel H A,et al.Light craft experiments in Germany[C]//Proc of SPIE.2000,4065:472-481.
[3] Myrabo L N,Messitt D G,Mead F B Jr.Ground and flight tests of a laser propelled vehicle[R].AIAA Paper,98-1001.
[4] 金星,洪延姬,崔村燕,等.激光推进冲量耦合系数的测量方法[J].强激光与粒子束,2004,16(7):861-864.(Jin X,Hong Y J,Cui C Y,et al.Measure method of impulse coupling-coefficient of laser propulsion.High Power Laser and Particle Beams,2004,16(7):861-864)
[5] 曹正蕊,洪延姬,李倩,等.单脉冲能量对光船推进性能的影响[J].热科学与技术,2005,4(2):183-188.(Cao Z R,Hong Y J,Li Q,et al.Influence of laser pulse energy on propulsion performance of lightcraft.Journal of Thermal Science and Technology,2005,4(2):183-188)
[6] 龚平,唐志平.大气呼吸模式激光推进的机理分析及数值模拟[J].爆炸与冲击,2003,23(6):501-508.(Gong P,Tang Z P.Mechanism analysis and numerical simulation of air-breathing model for laser propulsion.Explosion and Shock Waves,2003,23(6):501-508)
[8] Ageichik A A,Egorov M S,Ostapenko S V,et al.Experimental study on thrust characteristics of airspace laser propulsion engine[C]//CP702,Beamed Energy Propulsion:Second International Symposium on Beamed Energy Propulsion.2004:49-60.
[9] Ageichik A A,Egorov M S,Ostapenko S V,et al.Model test of the aerospace laser propulsion engine[C]//CP766,Beamed Energy Propulsion:Second International Symposium on Beamed Energy Propulsion.2005:183-194.
崔村燕, 洪延姬, 何国强, 李倩, 曹正蕊. 线性喷管构形对激光推力器冲量耦合系数的影响[J]. 强激光与粒子束, 2006, 18(2): 193. 崔村燕, 洪延姬, 何国强, 李倩, 曹正蕊. Influence of linear nozzle structure on impulse coupling coefficient of laser thruster[J]. High Power Laser and Particle Beams, 2006, 18(2): 193.