Abstract
C-SiC composite is a new type of material which is being developed with aerospace technology. C-SiC composite possesses excellent properties and can satisfy the requirements of spacecraft protection system. Therefore it is very significant to study the mechanical behavior of C-SiC composite subjected to hypervelocity impact. Based on current simulations and experiments about C-SiC composite, a set of parameters which are essential for simulating C-SiC composite subjected to hypervelocity impact are derived in this paper. The characteristics of C-SiC composite dual-wall shield under hypervelocity impact and its ballistic limit curve are obtained by numerical simulations with AUTODYN, and furthermore, the ballistic limit equation is also developed.
Original language | English |
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Pages (from-to) | 18-26 |
Number of pages | 9 |
Journal | Gaoya Wuli Xuebao/Chinese Journal of High Pressure Physics |
Volume | 26 |
Issue number | 1 |
State | Published - Feb 2012 |
Keywords
- Ballistic limit equation
- C-SiC composite
- Dual-wall structure
- Hypervelocity impact