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    G. S. Tussiwand, V. E. Saouma, R. Terzenbach, L. T. De Luca, Fracture mechanics of composite solid rocket propellant grains: Material testing, J. Propul. Power 2009, 25, 60.
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    P. H. Geubelle, H. M. Inglis, J. D. Kramer, J. J. Patel, N. C. Kumar, H. Tan, Multiscale modeling of dewetting damage in highly filled particulate composites, AIP Conf. Proc. 2008, 973, 196.
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    N. Niehaus, O. Greeb, Optimization of propellant binders-Part two: Macroscopic investgation of the mechanical properties of polymers, Propellants Explos. Pyrotech. 2004, 29, 333.
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    J. C. Li, Q. J. Jiao, H. Ren, D. Li, Preparation of NC-BA-RDX coating ball particles by means of layer-to-layer assembly technique, J. Solid Rocket Technol. 2008, 31, 247.
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    T. F. Nihal, U. B. Zühtü, The effect of ammonium nitrate, coarse/Fine ammonium nitrate ratio, plasticizer, bonding agent, and Fe2O3 content on ballistic and mechanical properties of hydroxyl terminated polybutadiene based composite propellants containing 20 % AP, J. ASTM Int. 2005, 2, 233.
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    A. A. Ali, J. W. Zhang, G. B. Cai, Investigation of the role of aziridine bonding agents on the aging of the composite solid rocket propellant (CSRP), J. Aerosp. Pow. 2008, 23, 2101.
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    J. Sciamareli, M. F. K. Takahashi, J. M. Teixeira, Solid polyurethane-based composite propellant: I – Influence of the bonding agent, Quim. Nova 2002, 25, 107.
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    X. H. Zhang, F. Q. Zhao, H. M. Tan, Improving mechanical property of CMDB propellant containing nitramine with bonding agent, Chinese J. Explos. Propell. 2005, 28, 1.
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    F. Q. Zhao, W. G. Shan, S. W. Li, Review on silane coupling agents used in solid rocket motor charges and their action mechanism, Energ. Mater. 1998, 6, 37.
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    H. Y. Zhang, Advances in low signature signal CMDB propellants, J. Solid Rocket Technol. 2000, 23, 36.
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    H. X. Tang, X. L. Liu, Q. Wu, Action mechanism of special functional agents in composite solid propellant. (IV) – Processability/mechanical properties, J. Solid Rocket Technol. 2004, 27, 193.
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    Y. Wang, G. Qiu, Thermal behavior of bonding agent 1,1-(1,3-phenylenedlcarbonyl) bis-2-methyl-aziridine, J. Propul. Technol. 2001, 22, 258.
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    L. Du, J. W. Xiao, R. K. Yin, Low temperature mechanical properties of high-burning rate HTPB/IPDI propellants (II) Design and application of surfactants, J. Propul. Technol. 2002, 23, 245.
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    H. X. Li, H. X. Tang, J. R. Deng, M. C. Zhou, Mechanism of PB aids added in nitrate plasticized propellants, J. Propul. Technol. 2002, 23, 164.
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    H. X. Tang, X. L. Liu, Q. Wu, Action mechanism of special functional agents in composite solid propellants (II) HTPB/Al system, J. Solid Rocket Technol. 2002, 25, 41.
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    T. S. Kokan, J. R. Olds, J. M. Seitzman, P. J. Ludovico, Characterizing high-energy-density propellants for space propulsion applications, J. Thermophys. Heat Transfer 2008, 22, 727.
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    X. F. Ma, W. H. Zhu, J. J. Xiao, H. M. Xiao, Molecular dynamics study of the structure and performance of simple and double bases propellants, J. Hazard. Mater. 2008, 156, 201.
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    W. S. Yao, Q. Li, H. M. Tan, Molecular simulation on properties of NEPE propellant binders, Chin. J. Energ. Mater. 2007, 15, 650.
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    G. C. Li, Y. G. Xing, Y. F. Wang, A. M. Pang, X. Guo, G. Tang, Micromechanical method of the effective modulus estimation for the composite propellant, J. Propul. Technol. 2007, 28, 441.
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    Y. C. Yang, D. M. Jiao, H. F. Qiang, G. Wang, Molecular simulation of solubility parameter for HTPB solid propellants, Chin. J. Energ. Mater. 2008, 16, 191.
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    B. F. Pan, Y. J. Luo, H. M. Tan, Study on interaction between CL-20 and dendritic bonding agent, Chin. J. Energ. Mater. 2004, 12, 199.
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    B. Zhang, Y. J. Luo, H. M. Tan, Interactional mechanism of the interface between CL-20 and some bonding agents, Chin. J. Explos. Propell. 2005, 28, 23.
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    J. C. Li, Q. J. Jiao, H. Ren, L. X. Wang, W. D. Zhao, RDX coated with hyantoin/triazines composite bonding agent, Chin. J. Energ. Mater. 2008, 16, 56.
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    Y. Yang, Y. J. Luo, Y. B. Jiu, M. N. Duo, Y. Lv, Z. Ge, Influence of CL-20 coated with thermoplastic polyurethane elastomers (TPU) on mechanical properties of NEPE propellant, J. Solid Rocket Technol. 2008, 31, 358.
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    H. B. Yang, W. Fu, L. X. Chang, M. H. Li, H. Bala, Q. J. Yu, G. T. Zou, Preparation and characteristics of core-shell structure nickel/silica nanoparticles, Colloids Surf. A 2005, 262, 71.