Simulation in the Reduction of Rocket Consumption in Multiple Launch Rocket System Tests

：Wang Guoping;Rui Xiaoting;Lu Yuqi;:Cheng Weidong;:Yun Laifeng

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  • Sponsored by: China Association for Science and Technology (CAST)

    Editor-In-Chief: Xu Yida

    ISSN 1000-1093

    　

  • Hosted By: China Ordnance Society

    Published By: Acta Armamentarii

    CN 11-2176/TJ

Acta Armamentarii, a Chinese monthly journal, was first published in 1979. The journal is supervised by China Association for Science and Technology, sponsored by China Ordnance Society，and edited and published by Editorial Board of Acta Armamentarii. The Journal is included in all important domestic databases，and also collected by Engineering Index (EI, USA), Chemical Abstracts (CA, USA), Science Abstracts (SA, UK）, Abstract Journal (AJ, Russia), and Current Bibliography on Science and Technology(CBST).Acta Armamentarii has been selected into the journal Of Ordnance Science and Technology (Weapons Industry) Field Of High Quality Scientific and Technological Periodical Classification Catalogue (2022 edition), ranking T1, and the journal of Automotive Engineering Field of High Quality Scientific and technological Periodical classification Catalogue, ranking T2.
Acta Armamentarii ›› 2004, Vol. 25 ›› Issue (6) : 786-789. DOI: 10.3969/j.issn.1000-1093.2004.06.030
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Simulation in the Reduction of Rocket Consumption in Multiple Launch Rocket System Tests

  • 1：Wang Guoping, Rui Xiaoting, Lu Yuqi;2:Cheng Weidong;3:Yun Laifeng
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Abstract

The theory of launch and flight dynamics in multiple launch rocket system (MLRs) is studied in some depth. Random integer programming is used and the simulation system in the reduction of rocket consumption in MLRS tests was developed. 7 tubes firing dispersion test scheme for a 40 tubes MLRS was presented using this simulation system. Lsmg the new scheme, rocket consumption is decreased by 82.5% . The scheme was strictly and directly verified by simulation results and contrastive firing tests. I tubes firing dispersion test scheme can be used to substitute for 40 tubes scheme in dispersion tests. Simula?tion in the reduction of rocket consumption in MLRS tests was further validated by oractical Iirmg tests.

Key words

computer application / multiple launch rocket system / rocket / simulation / random integer programming / test

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1：Wang Guoping, Rui Xiaoting, Lu Yuqi;2:Cheng Weidong;3:Yun Laifeng. Simulation in the Reduction of Rocket Consumption in Multiple Launch Rocket System Tests. Acta Armamentarii. 2004, 25(6): 786-789 https://doi.org/10.3969/j.issn.1000-1093.2004.06.030

References

[1] 阎章更,袁本信.武器弹药密集度试验分组比不分组好.兵工学报弹箭分册，1983，9(1):88?99
[2] 芮筱亭等.多体系统发射动力学.北京：国防工业出版社，1995. 10 ?69
[3] 徐明友.火箭外弹道学.北京:兵器工业出版社，1989. 133?163
[4] 芮筱亭等.多体系统传递矩阵法在火炮动力学中的应用.力学 与实践，1995,17(4):42 ?44
[5] 芮筱亭，杨启仁.弾丸发射过程理论.南京:东南大学出版社， 1991. 4 ?63
[6] 熊光楞，彭毅.先进仿真技术与仿真环境.北京：国防エ业出版 社，1997. 6-22

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