| 非化学平衡条件下膏体富燃料推进剂的热力计算 |
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| 引用本文： | 郑凯斌,陈林泉,张胜勇.非化学平衡条件下膏体富燃料推进剂的热力计算[J].火箭推进,2006,32(3):31-34. |
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| 作者姓名： | 郑凯斌 陈林泉 张胜勇 |
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| 作者单位： | 中国航天科技集团公司四院,陕西,西安,710025 |
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| 摘 要： | 膏体富燃料推进剂一次燃烧处于非平衡条件下,本文建立了非平衡条件下热力计算的理论模型以及不同热力学状态下求解平衡组分和燃烧温度的控制方程组。对给定配方的膏体富燃料推进剂在非平衡条件下的燃烧温度进行了计算,并对本文采用的方法进行了验证,证明是可行的。
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| 关 键 词： | 膏体富燃料推进剂 非化学平衡 热力计算 燃烧温度 |
| 文章编号： | (2006)03-0031-04 |
| 收稿时间： | 2005-12-08 |
| 修稿时间： | 2005-12-25 |
Thermodynamic calculation of fuel-rich pasty propellant under the chemical non-equilibrium condition |
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| Zheng Kaibin,Chen Linquan,Zhang Shengyong.Thermodynamic calculation of fuel-rich pasty propellant under the chemical non-equilibrium condition[J].Journal of Rocket Propulsion,2006,32(3):31-34. |
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| Authors: | Zheng Kaibin Chen Linquan Zhang Shengyong |
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| Abstract: | The primary combustion of fuel-rich pasty propellant is under the chemical non-equilibrium condition. This paper presents the theoretical model of thermodynamic calculation under the chemical non-equilibrium condition and equations solving equilibrium compositions and temperature in the different thermodynamic states. Nonequilibrium temperature is calculated for the given fuel-rich pasty propellant. The method adopted in this paper is compared with related result in other literature and it is shown that the method is feasible. |
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| Keywords: | fuel-rich pasty propellant chemical non-equilibrium thermodynamic calculation combustion temperature |
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