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Design and Experimental Study on Spinning Solid Rocket Motor

  • Conference paper
Artificial Intelligence and Computational Intelligence (AICI 2009)

Part of the book series: Lecture Notes in Computer Science ((LNAI,volume 5855))

Abstract

The study on spinning solid rocket motor (SRM) which used as power plant of twice throwing structure of aerial submunition was introduced. This kind of SRM which with the structure of tangential multi-nozzle consists of a combustion chamber, propellant charge, 4 tangential nozzles, ignition device, etc. Grain design, structure design and prediction of interior ballistic performance were described, and problem which need mainly considered in design were analyzed comprehensively. Finally, in order to research working performance of the SRM, measure pressure-time curve and its speed, static test and dynamic test were conducted respectively. And then calculated values and experimental data were compared and analyzed. The results indicate that the designed motor operates normally, and the stable performance of interior ballistic meet demands. And experimental results have the guidance meaning for the pre-research design of SRM.

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References

  1. Kamm, Y., Gany, A.: Solid Rocket Motor Optimization. In: 44th AAIA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, AIAA-2008-4695, Hartford, CT (2008)

    Google Scholar 

  2. French, J., Flandro, G.: Linked Solid Rocket Motor Combustion Stability and Internal Ballistic Analysis. In: 41st AAIA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, AIAA-2005-3998, Tucson, Arizona (2005)

    Google Scholar 

  3. Shimada, T., Hanzawa, M.: Stability Analysis of Solid Rocket Motor Combustion by Computational Fluid Dynamics. AIAA Journal 46(4), 947–957 (2008)

    Article  Google Scholar 

  4. Willcox, M.A., Brewster, Q., Tang, K.C.: Solid Rocket Motor Internal Ballistics Simulation Using Three-Dimensional Grain Burnback. Journal of Propulsion and Power 23(3), 575–584 (2007)

    Article  Google Scholar 

  5. Zhang, P., Zhang, W.S., Gui, Y.: Principle of Solid Rocket Motor. Beijing Institute of Science and Technology Press, Beijing (1992) (in Chinese)

    Google Scholar 

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Author information

Authors and Affiliations

  1. State Key Laboratory of Explosion Science and Technology, Beijing Institute of Technology, Beijing, China

    Heng Xue, Chunlan Jiang & Zaicheng Wang

Authors
  1. Heng Xue
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  2. Chunlan Jiang
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  3. Zaicheng Wang
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Editor information

Editors and Affiliations

  1. School of Business Information Technology, RMIT University, City Campus, 124 La Trobe Street, 3000, Melbourne, Victoria, Australia

    Hepu Deng

  2. College of Metrological Technology and Engineering, China Jiliang University, 310018, Hangzhou, Zhejiang Province, China

    Lanzhou Wang

  3. Department of Computer Science, City University of Hong Kong, 83 Tat Chee Avenue, Kowloon Tong, Hong Kong, China

    Fu Lee Wang

  4. College of Information Science and Technology, Hainan University, 570228, Haikou, China

    Jingsheng Lei

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© 2009 Springer-Verlag Berlin Heidelberg

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Xue, H., Jiang, C., Wang, Z. (2009). Design and Experimental Study on Spinning Solid Rocket Motor. In: Deng, H., Wang, L., Wang, F.L., Lei, J. (eds) Artificial Intelligence and Computational Intelligence. AICI 2009. Lecture Notes in Computer Science(), vol 5855. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-05253-8_78

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  • DOI: https://doi.org/10.1007/978-3-642-05253-8_78

  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-642-05252-1

  • Online ISBN: 978-3-642-05253-8

  • eBook Packages: Computer ScienceComputer Science (R0)

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