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第 46 卷 廖祜明,等: 预测不同冲击载荷下弹药响应特性的HOTM方法 第 3 期
Engineering, 2020, 41(5): 166–174. DOI: 10.11809/bqzbgcxb2020.05.032.
[2] NATO. Bullet attack test for munitions: NATO-STANAG 4241 [S]. NATO, 1991.
[3] United States Department of Defense. Hazard assessment tests for non-nuclear munitions: MIL-STD-2105C —2003 [S].
Department of Defense, 2003.
[4] NATO. Policy for introduction and assessment of insensitive munitions: STANAG 4439: 2010 [S]. NATO Standardization
Office, 2010.
[5] NATO. Guidance on the assessment and development of insensitive munitions (IM): AOP-39 [S]. NATO Standardization
Agency, North Atlantic Treaty Organization (NATO), 2010.
[6] 国防科学技术工业委员会. 炸药试验方法: GJB 772A—1997 [S]. 北京:国防科学技术工业委员会, 1997.
Explosive test method: GJB 772A—1997 [S]. Beijing: Commission of Science, Technology and Industry for National Defense
of the PRC, 1997.
[7] KIMURA E, OYUMI Y. Sensitivities of azide polymer propellants in fast cook-off, card gap and bullet impact tests [J].
Journal of Energetic Materials, 1997, 15(2/3): 163–178. DOI: 10.1080/07370659708216080.
[8] DAGLEY I J, HO S Y, NANUT V. Effects of the polymer matrix density on the shock, bullet impact and high strain-rate
ignition sensitivity of polymer bonded explosives [J]. Propellants, Explosives, Pyrotechnics, 1997, 22(5): 296–300. DOI:
10.1002/prep.19970220509.
[9] 魏祥庚, 刘佩进, 何国强, 等. HTPB 和 NEPE 固体推进剂枪击低易损性实验研究 [J]. 弹箭与制导学报, 2005, 25(4):
714–716. DOI: 10.3969/j.issn.1673-9728.2005.04.233.
WEI X G, LIU P J, HE G Q, et al. Experimental research on the low vulnerability of HTPB and NEPE solid propellant [J].
Journal of Projectiles, Rockets, Missiles and Guidance, 2005, 25(4): 714–716. DOI: 10.3969/j.issn.1673-9728.2005.04.233.
[10] 李小柱, 裴养卫. 固体火箭发动机枪击低易损性试验研究 [J]. 弹箭与制导学报, 2000(2): 39–42. DOI: 10.3969/j.issn.1673-
9728.2000.02.008.
LI X Z, PEI Y W. Low vulnerability experimental study of solid rocket engine under popping condition [J]. Journal of
Projectiles, Rockets, Missiles and Guidance, 2000(2): 39–42. DOI: 10.3969/j.issn.1673-9728.2000.02.008.
[11] 齐任超. 破片冲击作用下战斗部装药失效响应研究 [D]. 北京: 北京理工大学, 2015.
QI R C. Research on the low vulnerability method of warhead case under the impact of fragment [D]. Beijing: Beijing Institute
of Technology, 2015.
[12] 胡 杰 , 杜 剑 英 , 陈 桦 , 等 . 破 片 撞 击 不 敏 感 弹 药 研 究 进 展 [J]. 兵 器 装 备 工 程 学 报 , 2022, 43(8): 36–43. DOI:
10.11809/bqzbgcxb2022.08.006.
HU J, DU J Y, CHEN H, et al. Research progress of fragment impact insensitive ammunition [J]. Journal of Ordnance
Equipment Engineering, 2022, 43(8): 36–43. DOI: 10.11809/bqzbgcxb2022.08.006.
[13] JONES D A, KEMISTER G, BORG R A J. Numerical simulation of detonation in condensed phase explosives: DSTO-TR-
0705, AR-010-605 [R]. 1998.
[14] 代晓淦, 申春迎, 吕子剑, 等. 枪击试验中不同尺寸 PBX-2 炸药响应规律研究 [J]. 含能材料, 2008, 16(4): 432–435. DOI:
10.3969/j.issn.1006-9941.2008.04.017.
DAI X G, SHEN C Y, LÜ Z J, et al. Reaction properties for different size PBX-2 explosives in bullet impact test [J]. Chinese
Journal of Energetic Materials, 2008, 16(4): 432–435. DOI: 10.3969/j.issn.1006-9941.2008.04.017.
[15] 庄建华, 毛佳, 张为华, 等. 固体火箭发动机枪击过程数值模拟 [J]. 固体火箭技术, 2009, 32(4): 422–426. DOI:
10.3969/j.issn.1006-2793.2009.04.016.
ZHUANG J H, MAO J, ZHANG W H, et al. Numerical simulation of the gunshot process of solid rocket motor [J]. Journal of
Solid Rocket Technology, 2009, 32(4): 422–426. DOI: 10.3969/j.issn.1006-2793.2009.04.016.
[16] HAMAIDE S, QUIDOT M, BRUNET J. Tactical solid rocket motors response to bullet impact [J]. Propellants, Explosives,
Pyrotechnics, 1992, 17(3): 120–125. DOI: 10.1002/prep.19920170306.
[17] 濮赞泉. 破片撞击起爆战斗部影响因素及判据研究 [D]. 南京: 南京理工大学, 2016.
PU Z Q. Study on influencing factors and criterion of fragment impact initiation warhead [D]. Nanjing: Nanjing University of
Science and Technology, 2016.
[18] 刘沫言. 带壳装药的破片撞击和冲击波感度研究 [D]. 沈阳: 沈阳理工大学, 2020.
LIU M Y. Study on fragment impingement and shock wave sensitivity with shell charge [D]. Shenyang: Shenyang Ligong
034202-15

