| 提高固体火箭发动机性能的技术途径 |
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| 引用本文： | 曾妙胜.提高固体火箭发动机性能的技术途径[J].推进技术,1994,15(4):40-46. |
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| 作者姓名： | 曾妙胜 |
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| 作者单位： | 陕西动力机械研究所 |
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| 摘 要： | 用固体发动机比冲的理论计算方法计算了发动机比冲与平均工作压强的关系，由发动机质量比的表达式，推出质量比与发动机最大工作压强和平均工作压强比以及药柱装填分数的关系。计算和试验结果表明：发动机比冲随着平均工作压强增加而增加；发动机质量比随着药柱体积装填分数增加以及量大压强和平均压强比的减小而增加。结论：提高平均压强和药柱装填分数以及降低最大压强与平均压强比是提高发动机性能的技术途径。
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| 关 键 词： | 固体推进剂 火箭发动机 比冲 |
TECHNOLOGY METHODS TO IMPROVE SOLID ROCKET MOTOR PERFORMANCES |
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| Zeng Miaosheng.TECHNOLOGY METHODS TO IMPROVE SOLID ROCKET MOTOR PERFORMANCES[J].Journal of Propulsion Technology,1994,15(4):40-46. |
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| Authors: | Zeng Miaosheng |
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| Abstract: | The relation between motor specific impulse and average operating pressure is. calculated by using the theoretic calculating method of motor specific impulse. The relation between propellant-to-motor mass ratio and maximum operating pressure-to-average operating pressure ratio and grain volumetric loading fraction is inferred from the formula of propellant-to-motor mass ratio' It is shown by predication and tests that motor specific impulse rises with increase of average operating pressure and the propellant-to-motor mass ratio rises with the increase of grain volumetric loading fraction and the decrease of maximum pressure-to-average pressure ratio. |
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| Keywords: | Solid propellant rocket engine Propellant mass ratio Specific impulse Propellant grain |
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