参考文献/References:
[1]张国宏,黄少波,崔金平,等.固体火箭冲压发动机转级技术[J].弹箭与制导学报,2012,32(3):129-132.
ZHANG G H,HUANG S B, CUI J P,et al.Transition technology in integrated rocket ramjet engine[J].Journal of Projectiles,Rockets,Missiles and Guidance,2012,32(3):129-132.
[2] 叶定友.固体火箭冲压发动机的若干技术问题[J]. 固体火箭技术,2007,30(6):470-473.
YE D Y.Some technological problems of solid rocket ramjet[J].Journal of Solid Rocket Technology, 2007,30(6):470-473.
[3] 张全, 单睿子, 刘乐卿,等.一种先进的固体火箭冲压发动机堵盖设计[J].现代防御技术,2008,36(2):25-29.
ZHANG Q, SHAN R Z, LIU L Q,et al. Design of an advanced port cover for solid rocketramjet engine[J].Mo dern Defence Technology,2008,36(2):25-29.
[4]何德胜,李广武,杨威,等.固冲发动机三工况转级试验气流转换装置设计 [J].固体火箭技术,2012,35(3):419-422.
HE D S, LI G W, YANG W,et al.Design of air conversion device for threeoperating conditions conversion test of solid-fuel ramjet[J].Journal of Solid Rocket Technology,2012,35(3):419-422.
[5]祝逢春,徐振相,周彬,等. SCB火工品的研究与发展[J].爆破器材,2003,32(1):18-23.
ZHU F C, XU Z X, ZHOU B, et al. The research and development on semiconductor bridge initiator[J]. Explosive Materials,2003,32(1):18-23.
[6]高滨. 航天火工技术的现状和发展[J]. 航天返回与遥感,1999,20(3):63-67,62.
GAO B. The status and development of space pyrotechnics technique[J]. Spacecraft Recovery & Remote Sensing,1999,20(3):63-67,62.
[7] 张爱军,朱军伟,程时兵.一种基于DSP的半导体桥起爆电路的设计[J]. 火工品,2011(4):8-11.
ZHANG A J, ZHU J W, CHENG S B. Desing on semiconductor bridge initiating circuit based on DSP[J]. Initiators & Pyrotechnics,2011(4):8-11.
[8] 张文超,张伟,徐振相,等. 半导体桥的研究进展与发展趋势[J].爆破器材,2009,38(2):21-24.
ZHANG W C, ZHANG W, XU Z X, et al. Progress and development on semiconductor bridge initiator[J]. Explosive Materials,2009,38(2):21-24.
[9]黄少波,沈欣,李秋菊.空空导弹发动机点火系统安全性设计[J].航空兵器,2008(1):26-30.
HUANG S B, SHEN X, LI Q J.Safety design for the ignition system of air to air missile[J].Aero Weaponry,2008(1):26-30.