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[an error occurred while processing this directive]双脉冲发动机Ⅰ脉冲绝热材料二次烧蚀研究
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惠博(1979-),男,陕西西安人,高级工程师,研究方向:固体火箭发动机特种材料研究。 |
收稿日期: 2019-04-14
网络出版日期: 2025-02-12
Research on the Secondary Ablation of I Pulse Insulation Material in Double Pulse Solid Rocket
Received date: 2019-04-14
Online published: 2025-02-12
惠博 , 蒲德汉 , 刘伟凯 . 双脉冲发动机Ⅰ脉冲绝热材料二次烧蚀研究[J]. 弹箭与制导学报, 2020 , 40(3) : 35 -38 . DOI: 10.15892/j.cnki.djzdxb.2020.03.009
In order to obtain the second adiabatic characteristic of I pulse adiabatic materials at double pulse motor, and I pulse the second adiabatic device has been designed and two kind of erosion experiments have been done. Experiments and SEM results indicate the carbonized layer could not protect the adiabatic layer from ablation at higher II pulse flow velocity, the II pulse erosion rate is high obviously compare with I pulse of adiabatic materials erosion rate. While the adiabatic layer could not be removed at lower II pulse flow velocity, the carbonized layer could protect the adiabatic layer and the ablation rate of adiabatic layer would be decreased.
Key words: double pulse motor; insulation material; secondary ablation
| [1] |
张胜敏, 胡春波, 夏盛勇, 等. 高浓度颗粒流冲刷条件下硅橡胶和EPDM绝热材料动态烧蚀实验[J]. 推进技术, 2011, 32(2):241-244.
|
| [2] |
刘亚冰, 王长辉, 刘宇. 双脉冲发动机燃烧室局部烧蚀特性分析[J]. 固体火箭技术, 2011, 34(4):453-456.
|
| [3] |
孙娜, 娄永春, 孙长宏, 等. 某双脉冲发动机燃烧室两相流场数值分析[J]. 固体火箭技术, 2012, 35(3):335-338.
|
| [4] |
刘伟凯, 何国强, 王春光. 双脉冲固体火箭发动机压强振荡特性研究[J]. 航空动力学报, 2015, 30(10):2553-2560.
|
| [5] |
刘伟凯, 惠博. 双脉冲发动机中金属膜片式隔舱设计方法[J]. 固体火箭技术, 2013, 36(4):486-490.
|
| [6] |
何洪庆, 严红. EPDM的烧蚀模型[J]. 推进技术, 1999, 20(4): 37-40.
|
| [7] |
李江, 刘洋, 娄永春, 等. 颗粒冲刷对绝热层烧蚀影响的实验研究[J]. 推进技术, 2006, 27(1):71-73.
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