Improving Metallic Thermal Protection System Hypervelocity Impact Resistance Through Numerical Simulations-Reference-Cited by-同舟云学术

Improving Metallic Thermal Protection System Hypervelocity Impact Resistance Through Numerical Simulations

Published:2004-03 Issue:2 Volume:41 Page:221-231
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Poteet Carl C.¹,Blosser Max L.¹

Affiliation:

1. NASA Langley Research Center, Hampton, Virginia 23681

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.9193

Reference15 articles.

1. 1Blosser, M. L. "Advanced Metallic Thermal Protection Systems for Reusable Launch Vehicles," Ph.D. Dissertation, Dept. of Mechanical and Aerospace Engineering,Univ. of Virginia, Charlottesville, VA,May 2000.

2. 5Poteet, C. C. "Computational Study of Hypervelocity Impacts on Metallic Thermal Protection Systems," M.S. Thesis, School of Engineering and Applied Science,George WashingtonUniv., Washington,DC, Aug. 1998.

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