The Analysis of Non-coaxial Pintle Control Nozzle Thrust Performance and Influence Factor
Received date: 2012-12-17
Online published: 2025-05-26
唐金兰 , 胡博 , 李进贤 , 冯喜平 . 非同轴喉栓式推力调节喷管性能影响因素分析[J]. 弹箭与制导学报, 2013 , 33(4) : 123 -126 . DOI: 10.15892/j.cnki.djzdxb.2013.04.028
In order to study the performance of non-coaxial pintle control thrust nozzle, a method was proposed for calculating the nozzle equivalent throat area, and the analysis of influence by changes of different transition type face, shape of the pintle, angle of non coaxial and different diameter of the pintle was made. Conclusion: if the throat transition type face and shape of the pintle are straight line segment of the revolving body, thrust control will become linear, there is little influence of non-coaxial angle on thrust regulation: The effect of throat diameter on regulation is more effective, but in actual situation, proper size should be used.
| [1] | Susan L Burroughs Status of army pintle technology forcontrollable thrust propulsion, ΑΙΑΑ-2001-3598R, 2001. |
| [2] | 王毅林 喉栓式变推力固体发动机原理试验研究[D]. 西安: 西北工业大学, 2007. |
| [3] | 张淑慧, 胡波, 孟雅桃. 推力可控固体火箭发动机应用及发展. 固体火箭技术, 2002, 25 (4): 12- 15. |
| [4] | 滑利辉, 田维平, 甘晓松,等. 喉栓式推力可调发动机喷管流场数值模拟[J]. 固体火箭技术, 2008, 31 (4): 344- 349. |
| [5] | 李娟 喉栓发动机推力调节特性研究[D]. 西安: 西北工业大学, 2007. |
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