EPJ Web of Conferences
Volume 6, 2010ICEM 14 – 14th International Conference on Experimental Mechanics
|Number of page(s)||7|
|Section||Impact Mechanics and High Strain Rate|
|Published online||10 June 2010|
Damage Analysis for Hypervelocity Impact Experiments on Spaceship Windows Glass
Beijing Institute of Spacecraft Environment
5142-100, Beijing, 100094, P. R. China
2 China Academy of Space Technology, P.O.Box 5142, Beijing, 100094, P. R. China
a e-mail: firstname.lastname@example.org
The hypervelocity impact characteristics in fused silica glass, which is used for the outermost pane of the windshield as the critical part of the thermal protection system of spacecraft, were studied by 37 impact experiments with different millimeter diameter projectiles up to the velocity of 7 km/s launched by two stage light-gas-gun facility. The empirical damage equations were obtained from experiment data by the least square method and they were compared with NASA damage equations.
© Owned by the authors, published by EDP Sciences, 2010
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