Design and Structural Analysis of the Solid-State Recorder for Missile Flying Parameters Recording

Lei Feng; Tie Hua Ma

doi:10.4028/www.scientific.net/AMM.462-463.347

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 462-463Design and Structural Analysis of the Solid-State...

Design and Structural Analysis of the Solid-State Recorder for Missile Flying Parameters Recording

Abstract:

While the flying test of the missile, many kinds of parameters need to be recorded and the recording instruments are working in harsh environment. For this particular application a Solid-state recorder had been designed for obtaining and recording flying parameters of the missile, including data acquisition module, power management module, the central control module, a data storage module, the reading interface module, etc. Meanwhile, analyzed structures of the Solid-state recorder and completed thermal analysis and impact stress analysis of the structure using finite element analysis software ANSYS. The results had shown that the recorder can survive well in the flying test of the missile and the recorder had been applied to the actual trial and got accurate and reliable data.

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Periodical:

Applied Mechanics and Materials (Volumes 462-463)

Pages:

347-351

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.462-463.347

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Online since:

November 2013

Authors:

Lei Feng*, Tie Hua Ma

Keywords:

ANSYS, Flying Parameters, Missile, Solid-State Recorder, Structural Analysis

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* - Corresponding Author

References

[1] Zhang Wen-dong. Designing theory and applications of the storage test system [M]. Beijing: Higher Education Press, (2002).

Google Scholar

[2] Ao Miao. Large-capacity solid-state recorder with multi-channel [J]. Servo Control, 2012(1): 59-61.

Google Scholar

[3] Wen Feng, Ren Yong-feng, Wang Qiang. Design of a bomb-borne solid-state recorder for high-shock test and its application [J]. EXPLOSION AND SHOCK WAVES, 2009(2): 221-224.

Google Scholar

[4] Lu Hao, Wang Zhen-zhan. Design of High-rate Mass-capacity Solid-state Memory[J]. Computer Engineering, 2011(15): 226-231.

Google Scholar

[5] Feng Ni, Zhang Hui-xin, Lu Yi-nan, Liu Wen-yi. Hardware implementation of embedded AES encryption[J]. Video Engineering, 2013(3): 59-61.

Google Scholar

[6] Zhang Kai, Fan Jing-hui, Ma Yan, Huang Kun. Improving the toughness of epoxy resin encapsulating materials[J]. ELECTRONIC COMPONENTS & MATERIALS, 2011, 5(30): 65-67.

Google Scholar

[7] Zhao Feng-jun, Guo Min-qin. Research of epoxy potting adhesive used in appliances [J]. CHINA ADHESIVES, 1999, 8(1): 35-37.

Google Scholar