Abstract
With the purpose of further investigating the influence of aging on the tensile behaviors of hydroxyl-terminated polybutadiene (HTPB) propellant at low temperatures under dynamic loading, uniaxial tensile stress responses of thermal accelerated aged propellant samples at different temperatures (223–298 K) and strain rates (\(0.40\mbox{--}42.86~\mbox{s}^{-1}\)) were obtained through the use of a new INSTRON testing machine. And scanning electron microscope (SEM) was employed to analyze the microscopic damage of HTPB propellant under the test conditions. Test results indicate that aging can significantly affect the characteristics of the stress-strain curves, mechanical properties and fracture mechanisms of HTPB propellant at low temperatures under dynamic loading. There are three regions in the tensile stress-strain curves of aged propellant when deforming at lower temperatures and the highest strain rate, however, there are five ones for unaged propellant. At lower temperatures and higher strain rates, the strain at maximum tensile stress of the propellant decreases more obviously after aging. Moreover, the variation of mechanical parameters for HTPB propellant with aging time are highly complex due to the occurrence of oxidative cross-linking during aging and the distinct changes of the fracture mechanisms. These variation were reasonably well described with linear model and the improved exponential model in this investigation. The fracture mechanism of aged propellant can change from dewetting, matrix tearing and AP particle fracture to only AP particle fracture with increasing strain rate for the entire test temperature range, and the strain rate for this transition is all at \(4.00\mbox{--}14.29~\mbox{s}^{-1}\). In addition, the microscopic damage of HTPB propellant becomes more severe with the thermal aging time rising, however, this effect is weaker at higher strain rates after long-time thermal aging. Finally, the master curves of typical mechanical parameters for aged HTPB propellant were constructed according to the time-temperature superposition principle (TTSP).
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References
Andersen, P.C., Bruno, T.J.: Thermal decomposition kinetics of RP-1 rocket propellant. Ind. Eng. Chem. Res. 44(6), 1670–1676 (2005)
Bohn, M.A., Volk, F.: Aging behavior of propellants investigated by heat generation, stabilizer consumption, and molar mass degradation. Propellants Explos. Pyrotech. 17(4), 171–178 (1992)
Bunyan, P., Cunliffe, A.V., Davis, A., Kirby, F.A.: The degradation and stabilisation of solid rocket propellants. Polym. Degrad. Stab. 40(2), 239–250 (1993)
Celina, M., Minier, L., Assink, R.: Development and application of tools to characterize the oxidative degradation of AP/HTPB/al propellants in a propellant reliability study. Thermochim. Acta 384(1–2), 343–349 (2002)
Cerri, S., Bohn, M.A., Menke, K., Galfetti, L.: Ageing behaviour of HTPB based rocket propellant formulations. Central Eur. J. Energ. Mater. 6(2), 149–165 (2009)
Cerri, S., Bohn, M.A., Menke, K., Menke, K., Galfetti, L.: Aging of HTPB/Al/AP rocket propellant formulations investigated by DMA measurements. Propellants Explos. Pyrotech. 38(2), 190–198 (2013)
Chu, H.T., Chou, J.H.: Effect of cooling load on the safety factor of propellant grains. J. Propuls. Power 29(1), 27–33 (2013)
de la Fuente, J.L.: An analysis of the thermal aging behaviour in high-performance energetic composites through the glass transition temperature. Polym. Degrad. Stab. 94(4), 664–669 (2009)
de la Fuente, J.L., Rodrı´guez, O.: Dynamic mechanical study on the thermal aging of a hydroxyl-terminated polybutadiene-based energetic composite. J. Appl. Polym. Sci. 87(14), 2397–2405 (2015)
Deng, B., Tang, G., Shen, Z.: Structural analysis of solid rocket motor grain with aging and damage effects. J. Spacecr. Rockets 50(2), 331–339 (2015)
Edidin, A.A., Jewett, C.W., Kalinowski, A., Kwarteng, K., Kurtz, S.M.: Degradation of mechanical behavior in UHMWPE after natural and accelerated aging. Biomaterials 21(14), 1451–1460 (2000)
Gligorijević, N., Živković, S., Subotić, S., Rodić, V., Gligorijević, I.: Effect of cumulative damage on rocket motor service life. J. Energ. Mater. 33(4), 229–259 (2015)
Gligorijević, N.I., Rodić, V.Ž., Živković, S.Ž., Pavković, B.M., Nikolić, M.M., Kozomara, S.M., Subotić, S.D.: Mechanical characterization of composite solid rocket propellant based on hydroxy-terminated polybutadiene. Hem. Ind. 70(5), 581–594 (2016)
Goncalves, R.F.B., Silva, R.P., Rocco, J.A.F.F., Iha, K.: Thermal decomposition kinetics of aged solid propellant based on ammonium perchlorate-AP/HTPB binder. AIAA 2008-4969 (2008)
Hocaoğlu, Ö., Pekel, F., Özkar, S.: Aging of HTPB/AP-based composite solid propellants, depending on the NCO/OH and Triol/Diol ratios. J. Appl. Polym. Sci. 79(6), 959–964 (2001)
Husband, D.M.: Use of dynamic mechanical measurements to determine the aging behavior of solid propellant. Propellants Explos. Pyrotech. 17(4), 196–201 (1992)
Jalocha, D., Constantinescu, A., Neviere, R.: Prestrained biaxial DMA investigation of viscoelastic nonlinearities in highly filled elastomers. Polym. Test. 42, 37–44 (2015)
Jeremic, R.: Some aspects of time-temperature superposition principle applied for predicting mechanical properties of solid rocket propellants. Propellants Explos. Pyrotech. 24(4), 221–223 (1999)
Jiang, S.P., Rui, X.T., Hong, J., Wang, G.P., Rong, B., Wang, Y.: Numerical simulation of impact breakage of gun propellant charge. Granul. Matter 13, 611–622 (2011)
Judge, M.D.: An investigation of composite propellant accelerated ageing mechanisms and kinetics. Propellants Explos. Pyrotech. 28(3), 114–119 (2003)
Kadiresh, P.N., Sridhar, B.T.N.: Experimental evaluation and simulation on aging characteristics of aluminised AP-HTPB composite solid propellant. Mater. Sci. Technol. 24(4), 406–412 (2008)
Kadiresh, P.N., Sridhar, B.T.N.: Experimental study on ballistic behaviour of an aluminised AP/HTPB propellant during accelerated aging. J. Therm. Anal. Calorim. 100(1), 331–335 (2010)
Kishore, K., Paiverneker, V.R., Prasad, G.: Effect of storage temperatures on the mechanical properties of the composite solid propellants. Combust. Sci. Technol. 19, 107–118 (1979)
Kivity, M., Hartman, G., Achlama, A.M.: Aging of HTPB Propellant. AIAA 2005-3802 (2005)
Layton, L.H.: Chemical structural aging studies on HTPB propellant. ADA010731 (1975)
Lloyd, D.K.: Long-Range Service Life Analysis (LRSLA) estimating procedure. J. Spacecr. Rockets 14(6), 351–357 (1977)
Reeling Brouwer, G., Keizers, H.: Aging in composite propellant grains. AIAA 2004-4058 (2004)
Reeling Brouwer, G., Weterings, F.P., Keizers, H.: Evaluation of ageing in composite propellant grains: Part 2. AIAA 2005-3803 (2005)
Rocco, J., Lima, J., Frutuoso, A., Iha, K., Ionashiro, M., Matos, J., Suárez-Iha, M.: Thermal degradation of a composite solid propellant examined by DSC. J. Therm. Anal. Calorim. 75(2), 551–557 (2004)
Shekhar, H.: Studies on stress-strain curves of aged composite solid rocket propellants. Def. Sci. J. 62(2), 90–94 (2012)
Trache, D., Khimeche, K.: Study on the influence of ageing on chemical and mechanical properties of N,N’-dimethyl-N,N’-diphenylcarbamide stabilized propellants. J. Therm. Anal. Calorim. 111(1), 305–312 (2013)
Villar, L.D., Cicaglioni, T., Diniz, M.F., Takahashi, M.F.K., Rezende, L.C.: Thermal aging of HTPB/IPDI-based polyurethane as a function of NCO/OH ratio. Mater. Res. 14(3), 372–375 (2011)
Wang, Z., Qiang, H., Wang, G., Huang, Q.: Tensile mechanical properties and constitutive model for HTPB propellant at low temperature and high strain rate. J. Appl. Polym. Sci. 132(24) (2015a)
Wang, Z., Qiang, H., Wang, G.: Experimental investigation on high strain rate tensile behaviors of HTPB propellant at low temperatures. Propellants Explos. Pyrotech. 40(6), 814–820 (2015b)
Wang, Z., Qiang, H., Wang, G., Wang, T.: A new test method to obtain biaxial tensile behaviors of solid propellant at high strain rates. Iran. Polym. J. 25(6), 15–524 (2016a)
Wang, Z., Qiang, H., Wang, G., Zhu, Z.: Effects of low temperature and high strain rate on the tensile behaviors of high-performance energetic composite. In: MATEC Web of Conferences, vol. 67 (2016b)
Wang, Z., Qiang, H., Wang, T., Wang, G., Hou, X.: A thermovisco-hyperelastic constitutive model of HTPB propellant with damage at intermediate strain rates. Mech. Time-Depend. Mater. 22(3), 291–314 (2018)
Yıldırım, H.C., Özüpek, Ş.: Structural assessment of a solid propellant rocket motor: effects of aging and damage. Aerosp. Sci. Technol. 15(8), 635–641 (2011)
Zhao, Y.J., Zhang, W., Zhang, X.G., Zhu, H., Wang, C.H., Fang, L.J.: Aging property and storage life prediction of NEPE propellant. Theory Pract. Energ. Mater. 7(1), 163–166 (2007)
Zou, X., Uesaka, T., Gurnagul, N.: Prediction of paper permanence by accelerated aging comparison of the predictions with natural aging results. Cellulose 3(1), 269–279 (1996)
Zhou, D., Liu, X., Sui, X., Wei, Z., Wang, N.: Effect of pre-strain during ageing on the maximum elongation of composite solid propellants and its modelling. Polym. Test. 50, 200–207 (2016)
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The authors gratefully acknowledge the financial support of the National 973 Program in China (No. 61338) and the National Funds in China (Nos. 11772352, 61407200203 and 51328050101).
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Wang, Z., Qiang, H., Wang, T. et al. Tensile behaviors of thermal aged HTPB propellant at low temperatures under dynamic loading. Mech Time-Depend Mater 24, 141–159 (2020). https://doi.org/10.1007/s11043-019-09413-4
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DOI: https://doi.org/10.1007/s11043-019-09413-4