RDX/AP/HTPB复合推进剂老化的研究

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    Published By: Chinese Journal of Explosives & Propellants

    CN 61-1310/TJ

Chinese Journal of Explosives & Propellants ›› 1990, Vol. 13 ›› Issue (3) : 1-5,12.

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[1] 李君励.HMX相变特性及提高硝胺推进剂力学性能的途径.推进技术.1985(5),49
[2] 鲁念惠.复合固体推进剂研究动向(文献综述).国外固体火箭技术.1984 (3),43
[3] 贺南昌.复合固体推进剂的老化及防护.国防科技大学论文报告资料.1983
[4] Kishore K, Mechanism of Aging of composite solid propellant,Combustion Science and Technology, 1979, 19
[5] Christiansen A G, et al, HTPB Propellant Aging and Service Life,AIAA Paper 80-1273
[6] 吴国良,徐祥铭.复合固体推进剂相对交联键数目的测定.上海航天局806所科技报告.1982
[7] 夏竹苗.丁睛羟推进剂贮存寿命预估.航天部四院科技报告.1983
[8] 彭培根,贺南昌等.固体推进剂性能及原理.国防科技大学,1987
[9] 鲁念惠.复合固体推进剂的降解历程和使用寿命预测.推进技术.1985(6)

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