Improving Metallic Thermal Protection System Hypervelocity Impact Resistance Through Numerical Simulations
- 1 March 2004
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 41 (2) , 221-231
- https://doi.org/10.2514/1.9193
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Computational study of hypervelocity impacts on metallic thermal protection systemsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1998
- Theoretical equation of state for aluminumInternational Journal of Impact Engineering, 1987
- An overview of the theory of hydrocodesInternational Journal of Impact Engineering, 1987