[1] 侯林法,等.复合固体推进剂[M].北京:宇航出版社,1994:349-350. [2] 张炜,等.火箭推进剂[M].北京:国防工业出版社,2014:143-144. [3] LOYD D K.Long range service life analysis(LRSLA)system trend analysis life estimating procedure[R]. Cincinnati,OH:AIAA,1976. [4] HUBNER C,GEIBLER E,ELSNER P.The importance of micromechanical phenomena in energetic material[J]. Propellant,Explosives,Pyrotechnics,1999,24(3):119-125. [5] JIMMY D C,SEEMA S,DARRYL Y S,et al. Autonomous optical sensor system for the monitoring of nitrogen dioxide from aging rocket propellant[R].SAND2001-2953,2001. [6] HUANG Weidong.Mechanical property prediction method for a htpb propellant aging[R].Cincinnati,OH:AIAA,2007. [7] SARA Cerri,MANFRED A.Bohn,KLAUS Menke.Aging of HTPB/AI/AP rocket propellant formulations investigated by DMA measurements propellant[J].Explosives,Pyrotechnics, 2013,38(2):190-198. [8] NEVIERE R,GUYADER M.DMA:a powerful technique to assess ageing of MED[C]//37th International Annual Conference of ICT.Karlsruhe,Germany,2006. [9] STEPHENS W D,SCHWARZ W W,KRUSE R B,et al.Application of fourier transform spectroscopy to propellant service life prediction[R].Cincinnati,OH:AIAA,1976. [10] DUNCAN E J S.Characterization of glycidyl azide ploymer composite propellant:strain rate effects and relaxation response[J].Journal of Applied Polymer Science,1995,56(3):365-375. [11] DUNCAN E J S,BROUSSEAU P.Comparison of the uniaxial tensile modulus and dynamic shear storage modulus of a filled ahaydroxyl-terminated polybutadiene and GAP propellant[J].Journal of Materials Science,1996,31(5):1275-1284. [12] 阳建红,俞茂宏,侯根良,等.HTPB复合固体推进剂含损伤和老化本构研究[J].推进技术,2002,23(06):509-512. [13] 张昊,庞爱民,彭松.方坯药预测寿命与发动机推进剂药柱实际寿命差异研究[J].固体火箭技术,2005,28(01):53-56. [14] 李松年,刘勇,王罗新,等.HTPB推进剂储存老化性能试验研究[J].推进技术,2006,27(5):473-476. [15] 丁彪,张旭东,刘著卿,等.HTPB推进剂交变温度加速老化与自然贮存相关性[J].含能材料,2011,19(1):50-54. [16] 唐国金,申志彬,田四朋,等.固体火箭发动机药柱概率贮存寿命预估[J].兵工学报,2012,33(3):301-306. [17] 庞爱民.固体火箭推进剂理论与工程[M].北京:中国宇航出版社,2014:527-528. [18] CELINA M,GILLEN K T,ASSINK R A.Accelerated aging and lifetime prediction:review of non-Arrhenius behaviour due to two competing processes[J].Polymer Degradation & Stability,2005,90(3):395-404. [19] CELINA M,GRAHAM AC,GILLEN KT,et al.Thermal degradation studies of a polyurethane propellant binder[J]. Rubber Chemistry & Technology,2000,73(4):678-693. [20] CELINA M,WISE J,OTTESEN DK,et al.Correlation of chemical and mechanical property changes during oxidative degradation of neoprene[J].Polymer Degradation & Stability,2000,68(99):171-184. [21] GILLEN KT,CELINA M,BEMSTEIN R.Review of the ultrasensitive oxygen consumption method for making more reliable extrapolated predictions of polymer lifetimes[J].Ann Tech.Conf.Soc.Plast.Eng.,2004,62(2):2289-2293. [22] BEMSTEIN R,DERZON D K,GILLEN K T.Nylon 6.6 accelerated aging studies:thermal-oxidative degradation and its interaction with hydrolysis[J].Polymer Degradation & Stability,2005,88(3):480-488. [23] 陈西战,徐颖军,王鹏.基于凝胶百分数的推进剂贮存寿命及其可靠性分析[J].火工品,2007(1):1-4. [24] 王国强,史爱娟,丁黎,等.丁羟推进剂的热加速老化力学性能及寿命预估[J].火炸药学报,2015,38(1):47-50. [25] 高大元,何碧,何松伟,等.Arrhenius方法的局限性讨论[J].含能材料,2006,14(2):132-135. [26] GILLEN KT,BEMSTEIN R,CELINA M.Non-Arrhenius behavior for oxidative degradation of chlorosulfonated polyethylene materials[J].Polymer Degradation & Stability,2005,87(2):335-346. [27] GILLEN KT,BEMSTEIN R,DERZON D K.Evidence of non-Arrhenius behavior from laboratory aging and 24-year field aging of polychloroprene rubber materials[J].Polymer Degradation & Stability,2005,87(1):57-67. [28] GILLEN KT,CELINA M.The wear-out approach for predicting the remaining lifetime of materials[J].Office of Scientific & Technical Information Technical Reports,2000,71(1):15-30. [29] El-MAZRY C,HASSINE M B,CORREC O,et al. Thermal oxidation kinetics of additive free polyamide 6-6[J]. Polymer Degradation & Stability,2013,98(1):22-36. [30] 陈海建,滕克难,李波,等.基于修正Arrhenius方法的SRM药柱储存寿命预估[J].弹箭与制导学报,2011,31(04):232-235. [31] 傅惠民,杨立保,林逢春,等.固体推进剂贮存寿命整体预测方法[J].机械强度,2007,29(5):754-759. [32] 张昊,罗怀德,杜娟.线性活化能法预估推进剂贮存寿命研究[J].固体火箭技术,2002,25(2):56-58. [33] LAYTON L.Chemical structural aging studies on HTPB propellant[R].AD-A010731,1975. [34] CUNLIFFE A V,TOD QINETIQ D A,SEVENOAKS G B.Sol fraction measurements-a tool to study cross-linking and ageing in composite propellant and PBXs[C]//37th International Annual Conference of ICT.Karlsruhe,Germany,2006. [35] 王春华,彭网大,翁武军,等.HTPB推进剂贮存寿命的理论预估[J].推进技术,2000,21(3):63-66. [36] 罗怀德,张昊,杜娟.固体推进剂使用寿命快速预测探索研究[J].固体火箭技术,2000,23(1):31-35. [37] 杨根,赵永俊,张炜,等.HTPB推进剂贮存期预估模型研究[J].固体火箭技术,2006,29(4):283-285. [38] 杨根.N-15B推进剂热老化特性与贮存寿命预估研究[D].长沙:国防科学技术大学,2005. [39] 庄建华,刘纪涛,张为华,等.高能固体推进剂贮存寿命可靠性评估[J].弹箭与制导学报,2008,28(3):169-172. [40] 杨继坤,徐廷学,董琪,等.固体火箭发动机装药贮存寿命预测方法[J].推进技术,2013,34(3):416-421. [41] ANDERS Thorin.Influence of prestrain on mechanical properties of highly-filled elastomers:measurements and modeling[J].Polymer Testing,2012,31(8):978-986. [42] 张昊,彭松,庞爱民.固体推进剂应力和应变与使用寿命关系[J].推进技术,2006,27(4):372-375. [43] 邹思斯,严聪,马岑睿,等.定应变下HTPB推进剂延伸率二元回归模型[J].弹箭与制导学报,2013,33(4):131-133. [44] 张磊,常新龙,赖建伟.基于湿热加速老化试验的HTPB固体推进剂寿命预估[J].弹箭与制导学报,2010,30(1):148-150. [45] 李进贤,莫文宾,唐金兰.固体推进剂力学性能预估研究[J].计算机仿真,2011,28(1):76-79. [46] CELINA M,WISE J,OTTESEN D K,et al.Oxidation profiles of thermally aged nitrile rubber[J].Polymer Degradation & Stability,1998,60(2):493. [47] CELINA M C,DAYILE A R,QUINTANA A.A perspective on the inherent oxidation sensitivity of epoxy materials[J].Polymer,2013,54(13):3290-3296. [48] WISE J,GILLEN K T,CLOUGH R L.Quantitative model for the time development of diffusion-limited oxidation profiles[J].Polymer,1997,38(8):1929-1944. [49] BERTRAND Roduit,MARCO Hartmann,PATRICK Folly,et al.Prediction of thermal stability of materials by modified kinetic and model selection approaches based on limited amount of experimental point[J].Thermochimica Acta,2014,579(5):31-39. [50] 周洁,姚军,宋燕.基于分段非线性Arrhenius的贮存寿命评估方法[J].北京航空航天大学学报,2015,41(4):744-750. |