Improvement and optimal design of a seat-buffer system in reentry capsule of spacecraft

LI Dao-kui;LIAO Yi-huan;XIE Yan;TANG Guo-jin

Journal of Vibration and Shock ›› 2009, Vol. 28 ›› Issue (11) : 107-109.

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PDF(1208 KB)
Journal of Vibration and Shock ›› 2009, Vol. 28 ›› Issue (11) : 107-109.
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Improvement and optimal design of a seat-buffer system in reentry capsule of spacecraft

  • LI Dao-kui, LIAO Yi-huan, XIE Yan, TANG Guo-jin
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Abstract

A new plan is presented to improve the performance of seat-buffer system of reentry capsule. The articulated sustentation is changed into sideling elastic sustentation. The dynamics model of seat-buffer system is established using ADAMS. With method of parameterized modeling, optimal design for the parameters of sideling elastic sustentation is accomplished. The dynamic simulation results of the optimized seat-buffer system show that the optimized seat-buffer system not only decrease the shock response along chest-back direction, but also observably reduces the shock response along head-ilium direction compared with the former system.

Key words

seat-buffer system / optimal design / dynamics simulation / ADAMS

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LI Dao-kui;LIAO Yi-huan;XIE Yan;TANG Guo-jin. Improvement and optimal design of a seat-buffer system in reentry capsule of spacecraft[J]. Journal of Vibration and Shock, 2009, 28(11): 107-109
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