Burning Rate Dependence of Composite Propellants on Ammonium Perchiorate Particle Size

摘要：

The experimental measured results show a wide variation in the burning rate with change in AP mean diameter. The resultant trend is a typical S shaped curve which is the characteristic of AP propellants having stoichiometric oxidizer to fuel ratios or fuel rich compositions. A simplified model is developed to calculate the propellant burning rates based on the multiple flames model concept. The computed burning rates are compared with the experimental results and good agreement is found.

关键词： composite propellant ammonium perchiorate combustion burning rate particle size

作者: Muhammad Mazhar IQBAL Sajid RAZA Ch.

作者单位: National Engineering and Scientific Commission, Islamabad, Pakistan

会议类型: 国际会议

会议名称: 2007国际推进剂、炸药、烟火技术秋季研讨会(The 2007 International Autumn Seminar on Propellants,Explosives and Pyrotechnics)

会议地点: 西安

会议语种:英文

页码: 376-380

在线出版日期: 2007-10-23（万方平台首次上网日期，不代表论文的发表时间）