摘要
Thermoplastic polyurethane (TPU) was coated on the hexanitrohexaazaisowurtzitane (CL-20) by means of water-solution suspension method. The coated CL-20 were tested by means of XPS, SEM, impact sensitivity and surface free energy measurement methods. The effects of the coated CL-20 on mechanical and combustion properties of NEPE propellant at room temperature were investigated. The results show that the coated CL-20 can greatly improve mechanical properties of NEPE propellant at room temperature as well as demoisture and combustion properties of high energy low characteristic signal propellant; σm can maximally increase by 47% and εm can increase by 184%, the pressure exponent n can decrease by 12%.
源语言 | 英语 |
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页(从-至) | 358-362+373 |
期刊 | Guti Huojian Jishu/Journal of Solid Rocket Technology |
卷 | 31 |
期 | 4 |
出版状态 | 已出版 - 8月 2008 |