Articles | Volume 10, issue 1
https://doi.org/10.5194/ms-10-71-2019
https://doi.org/10.5194/ms-10-71-2019
Research article
 | 
15 Feb 2019
Research article |  | 15 Feb 2019

Design and dynamic analysis of metal rubber isolators between satellite and carrier rocket system

Xibin Cao, Cheng Wei, Jiqiu Liang, and Lixu Wang

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Cited articles

Bishop, R. E. D.: Mechanical Vibration, Nature, 182, 1581–1581, 1958. 
Cao, F., Bao, H., Ren, G., and Fan, H.: Constitutive Model of Metal Rubber Material Based on Curved Cantilever Beam of Variable Length, J. Mech. Eng., 48, 61–66, 2012. 
Holtz, M.: Modeling and Design of a Novel Air-spring for a Suspension Seat, J. Sound Vib., 329, 4354–4366, 2010. 
Ibrahim, R. A.: Recent advances in nonlinear passive vibration isolators, J. Sound Vib., 314, 371–452, 2008. 
Johnson, C. D.: Design of Passive Damping Systems, J. Vib. Acoust., 117, 171–176, 1995. 
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Short summary
For launching satellite, with the needs of mobility and rapid-responsibility, the vehicle is used for launching. The system inevitably undergoes random vibrations caused by uneven ground excitation, while the camera and other high-precision payloads of the satellite cannot withstand the harsh mechanical environment without isolators. Due to the superior damping properties of MR, this paper designs the simple MR components and provides a feasible design method to absorb vibrations.