[1] Pakhomov A V, Gregory D A, Thompson M S. Specific impulse and other characteristics of elementary propellants for ablative laser propulsion. AIAA Journal, 2002,40(5):947～952

[2] Pakhomov A V, Gregory D A. Ablative laser propulsion: an old concept revisited. AIAA Journal, 2000,38(4):725～727

[3] Myrabo L N, Messitt D G, Mead F B. Ground and flight test of a laser propelled vehicle AIAA. 1998, 98-1001:12～16

[4] Phipps C R, Michaells M M. LISP, J. Laser and particle beams. 1994,12(1):23～24

[5] Shigeaki U, Xianglin Z, Kanzuo I. Study on momentum coupling efficiency of laser ablation for space debris removal. SPIE,2000,3885:65～71

[6] Glumb R J, Krier H. Concepts and status of laser-supported rocket propulsion. J. Spacecraft and rockets, 1984,21(1):70～79

[7] Pakhomov A V ,Gregory D A. Ablative laser propulsion: An advanced concept for space transportation, 2000 Young Faculty Research Proceedings, The University of Alabama in Huntsville, 2000,63～72

[8] Kantrowitz A. Propusion to orbit by ground-based lasers. Astronautics and Aeronautics, 10(5):74～76

[9] Myrabo L N, Messitt D G, Mead F B. Flight experiments and evolutionary development of a laser propelled,trans-atmospheric vehicle. SPIE, 1998,3343:560～563

[10] Bohn W L. Laser lightcraft performance. SPIE, 2000,3885:48～53

[11] Phipps C R, Reilly J P, Campbell J W. Optimum parameters for laser-launching objects into low earth orbit, J. Laser and particle beams. 2001,2:1～38

[12] 林敏华.以激光推进航天飞行器.国外激光,1991,16(2):43

[13] Yabe T, Phipps C, Yamaguchi M et al., Microairplane propelled by laser driven exotic target. Applied Physics Letters, 2002,80(23):4318～4320

[14] 郭振华,许德胜.高功率密度激光辐射效应.激光技术,1989,13(5):15～20

[15] 程祖海,王新兵,王又青.激光推进的理论及实验研究.激光与光电子学进展,2001,(9):39

[16] Chongyi Wan, Shiming Liu, Jinwen Zhou et al., High repetition rate industrial TEA CO2 laser with output power of 1.5kW.SPIE, 1994,2502:87～89

[17] 郭大浩,吴鸿兴,王声波等,用激光推进轻型飞行器的初步实验探索.激光与光电子学进展,2001,(9):30