Internal ballistic calculation and test study on spinning solid rocket motor

Heng Xue; Chunlan Jiang; Zaicheng Wang

doi:10.1109/ICICTA.2009.443

Internal ballistic calculation and test study on spinning solid rocket motor

Heng Xue^*, Chunlan Jiang, Zaicheng Wang

^*Corresponding author for this work

School of Mechatronical Engineering

Beijing Institute of Technology

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

3 Citations (Scopus)

Abstract

Interior ballistic model of spinning solid rocket motor (SRM) and a method of internal ballistic calculation were presented in this paper. The internal ballistic calculation equations were solved by fourth-order runge-kutta method. The calculation program and the law of pressure along with time were obtained. Through contrasting with test data, correctness of the theoretical model was verified. Finally, experimental methods and data disposal were discussed. The results indicate that the designed motor operates normally, the interior ballistic performance meets requirements, and the experiment can be done repeat. Furthermore, the experimental results have the guidance meaning for the pre-research design of spinning SRM.

Original language	English
Title of host publication	2009 2nd International Conference on Intelligent Computing Technology and Automation, ICICTA 2009
Pages	860-863
Number of pages	4
DOIs	https://doi.org/10.1109/ICICTA.2009.443
Publication status	Published - 2009
Event	2009 2nd International Conference on Intelligent Computing Technology and Automation, ICICTA 2009 - Changsha, Hunan, China Duration: 10 Oct 2009 → 11 Oct 2009

Publication series

Name	2009 2nd International Conference on Intelligent Computing Technology and Automation, ICICTA 2009
Volume	2

Conference

Conference	2009 2nd International Conference on Intelligent Computing Technology and Automation, ICICTA 2009
Country/Territory	China
City	Changsha, Hunan
Period	10/10/09 → 11/10/09

Keywords

Igniter
Internal ballistic calculation
Solid rocket motor
Static test

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10.1109/ICICTA.2009.443

Cite this

Xue, H., Jiang, C., & Wang, Z. (2009). Internal ballistic calculation and test study on spinning solid rocket motor. In 2009 2nd International Conference on Intelligent Computing Technology and Automation, ICICTA 2009 (pp. 860-863). Article 5287829 (2009 2nd International Conference on Intelligent Computing Technology and Automation, ICICTA 2009; Vol. 2). https://doi.org/10.1109/ICICTA.2009.443

@inproceedings{de59afab45d8497187b0e8e775ed10e9,

title = "Internal ballistic calculation and test study on spinning solid rocket motor",

abstract = "Interior ballistic model of spinning solid rocket motor (SRM) and a method of internal ballistic calculation were presented in this paper. The internal ballistic calculation equations were solved by fourth-order runge-kutta method. The calculation program and the law of pressure along with time were obtained. Through contrasting with test data, correctness of the theoretical model was verified. Finally, experimental methods and data disposal were discussed. The results indicate that the designed motor operates normally, the interior ballistic performance meets requirements, and the experiment can be done repeat. Furthermore, the experimental results have the guidance meaning for the pre-research design of spinning SRM.",

keywords = "Igniter, Internal ballistic calculation, Solid rocket motor, Static test",

author = "Heng Xue and Chunlan Jiang and Zaicheng Wang",

year = "2009",

doi = "10.1109/ICICTA.2009.443",

language = "English",

isbn = "9780769538044",

series = "2009 2nd International Conference on Intelligent Computing Technology and Automation, ICICTA 2009",

pages = "860--863",

booktitle = "2009 2nd International Conference on Intelligent Computing Technology and Automation, ICICTA 2009",

note = "2009 2nd International Conference on Intelligent Computing Technology and Automation, ICICTA 2009 ; Conference date: 10-10-2009 Through 11-10-2009",

}

Xue, H, Jiang, C & Wang, Z 2009, Internal ballistic calculation and test study on spinning solid rocket motor. in 2009 2nd International Conference on Intelligent Computing Technology and Automation, ICICTA 2009., 5287829, 2009 2nd International Conference on Intelligent Computing Technology and Automation, ICICTA 2009, vol. 2, pp. 860-863, 2009 2nd International Conference on Intelligent Computing Technology and Automation, ICICTA 2009, Changsha, Hunan, China, 10/10/09. https://doi.org/10.1109/ICICTA.2009.443

Internal ballistic calculation and test study on spinning solid rocket motor. / Xue, Heng; Jiang, Chunlan ; Wang, Zaicheng.
2009 2nd International Conference on Intelligent Computing Technology and Automation, ICICTA 2009. 2009. p. 860-863 5287829 (2009 2nd International Conference on Intelligent Computing Technology and Automation, ICICTA 2009; Vol. 2).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

TY - GEN

T1 - Internal ballistic calculation and test study on spinning solid rocket motor

AU - Xue, Heng

AU - Jiang, Chunlan

AU - Wang, Zaicheng

PY - 2009

Y1 - 2009

N2 - Interior ballistic model of spinning solid rocket motor (SRM) and a method of internal ballistic calculation were presented in this paper. The internal ballistic calculation equations were solved by fourth-order runge-kutta method. The calculation program and the law of pressure along with time were obtained. Through contrasting with test data, correctness of the theoretical model was verified. Finally, experimental methods and data disposal were discussed. The results indicate that the designed motor operates normally, the interior ballistic performance meets requirements, and the experiment can be done repeat. Furthermore, the experimental results have the guidance meaning for the pre-research design of spinning SRM.

AB - Interior ballistic model of spinning solid rocket motor (SRM) and a method of internal ballistic calculation were presented in this paper. The internal ballistic calculation equations were solved by fourth-order runge-kutta method. The calculation program and the law of pressure along with time were obtained. Through contrasting with test data, correctness of the theoretical model was verified. Finally, experimental methods and data disposal were discussed. The results indicate that the designed motor operates normally, the interior ballistic performance meets requirements, and the experiment can be done repeat. Furthermore, the experimental results have the guidance meaning for the pre-research design of spinning SRM.

KW - Igniter

KW - Internal ballistic calculation

KW - Solid rocket motor

KW - Static test

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U2 - 10.1109/ICICTA.2009.443

DO - 10.1109/ICICTA.2009.443

M3 - Conference contribution

AN - SCOPUS:71949123224

SN - 9780769538044

T3 - 2009 2nd International Conference on Intelligent Computing Technology and Automation, ICICTA 2009

SP - 860

EP - 863

BT - 2009 2nd International Conference on Intelligent Computing Technology and Automation, ICICTA 2009

T2 - 2009 2nd International Conference on Intelligent Computing Technology and Automation, ICICTA 2009

Y2 - 10 October 2009 through 11 October 2009

ER -

Internal ballistic calculation and test study on spinning solid rocket motor

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