Research Article
Numerical Simulation of Projectile Oblique Impact on Microspacecraft Structure
Table 3
Experiment and simulation results of rear face sheet of honeycomb sandwich panel.
| | | Projectile diameter/mm | Velocity/km·s−1 | Experiment result/mm | Simulation result/mm | Error |
| | Test 1 | 5 | 1.915 | 14.1 | 15.3 | 7.8% | | Test 2 | 8 | 1.7 | 22.5 | 24.6 | 8.5% | | Test 3 | 5 | 3.065 | 25.4 | 23.9 | 5.9% |
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