[1] 刘磊力,李凤生,支春雷,等.镁基储氢材料对AP/Al/HTPB复合固体推进剂性能的影响[J].含能材料, 9,7(5):501-504.
[2] 罗运军,李国平,刘晶如.一种以储氢合金为燃烧剂的固体推进剂[P].中国国防发明专利:7.zl200710081890.6,2007.
[3] 刘晶如,罗运军.贮氢合金燃烧剂与固体推进剂常用含能组分的相容性研究[J].兵工学报,8,9(9).
[4] 刘晶如,罗运军.含储氢合金的丁羟推进剂固化气孔问题研究[J].固体火箭技术,1,4(1):92-96.
[5] 刘晶如,罗运军.固体推进剂用铝基复合材料的制备及性能[J].固体火箭技术, 0,3(5):545-548.
[6] 窦燕蒙,李国平,罗运军,等.储氢合金燃烧剂基本性能研究[J].固体火箭技术,1,4(6):760-763.
[7] 陈沛,赵凤起,阴翠梅.RDX/AP/HTPB推进剂热分解特性研究[J].固体火箭技术,2002,25(2):52-55.
[8] Pace K K, Jarymowycz T A, Yang V, et al.Effect of Magnesium-Coated Boron Particles on Burning Characteristics of Fuels in High-speed Cross Flows[M].Germany:CRC Press,1993:332-346.
[9] Mota J M, Abenojar J, Martinez M A.Effect of the Addition of Mechanically Alloyed Fe-B (wt50%)on the High Energy Composite Propellants, Born Based Sintered[C].Germany:34th International Annual Conference of ICT,2003:1-10.
[10] Dreizin E L, Keil D G, Felder W.Phase Changes in Boron Iignition and Combustion[J].Combustion and Flame, 9,9:272-290.
[11] 张瑞庆.固体火箭推进剂[M].北京:兵器工业出版社,1991.
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