Synthesis of three novel laurylamine-derived long-chain alkyl bonding agents and their interactions with RDX

Propellants, Explosives, Pyrotechnics

Volumn 37, Issue 1, 2012, Pages 69-76

  Liu, Yun Fei ^a   Chen, Yu ^a   Shi, Liang ^b   Yao, Wei Shang ^a  

^a BEIJING INSTITUTE OF TECHNOLOGY   (China)

^b Kingfa Science and Technology Company   (China)

Author keywords

Bonding agents; Interactions; Laurylamine; Mechanical properties; RDX

Indexed keywords

ALKYL BONDING; BINDER MATRIX; BONDING AGENT; CHARACTERISTIC ABSORPTION; EXPERIMENTAL DATA; FILLING PARTICLES; INTERACTION ENERGIES; LAURYLAMINE; MOLECULAR DYNAMICS METHODS; MOLECULAR DYNAMICS SIMULATIONS; RDX; SOLID PARTICLES; STRONG INTERACTION;

ADHESION; ADHESIVES; BEAM PLASMA INTERACTIONS; INFRARED SPECTROSCOPY; MECHANICAL PROPERTIES; MOLECULAR DYNAMICS;

SOLID PROPELLANTS;

EID: 84863164114     PISSN: 07213115     EISSN: 15214087     Source Type: Journal    
DOI: 10.1002/prep.201100014     Document Type: Article

References (26)

1. P.D. Gilbert, Multifunctional additives for composite solid propellant, MSc Thesis, Purdue University, 2008.
2. G.S. Tussiwand, V.E. Saouma, R. Terzenbach, L.T. DeLuca, Fracture mechanics of composite solid rocket propellant grains: Material testing, J. Propul. Power 2009, 25, 60.
3. 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.
4. N. Niehaus, O. Greeb, Optimization of propellant binders-Part two: Macroscopic investgation of the mechanical properties of polymers, Propellants Explos. Pyrotech. 2004, 29, 333.
5. 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.
6. 3 content on ballistic and mechanical properties of hydroxyl terminated polybutadiene based composite propellants containing 20% AP, J. ASTM Int. 2005, 2, 233.
7. 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.
8. 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.
9. 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.
10. 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.
11. H.Y. Zhang, Advances in low signature signal CMDB propellants, J. Solid Rocket Technol. 2000, 23, 36.
12. 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.
13. Y. Wang, G. Qiu, Thermal behavior of bonding agent 1,1-(1,3- phenylenedlcarbonyl) bis-2-methyl-aziridine, J. Propul. Technol. 2001, 22, 258.
14. 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.
15. 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.
16. 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. (Pubitemid 35347432)
17. 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.
18. 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.
19. W.S. Yao, Q. Li, H.M. Tan, Molecular simulation on properties of NEPE propellant binders, Chin. J. Energ. Mater. 2007, 15, 650.
20. 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.
21. 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.
22. 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.
23. 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.
24. 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.
25. 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.
26. 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.