Material Characterization of Shuttle Thermal Protection System for Impact Analyses-Reference-Cited by-同舟云学术

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Material Characterization of Shuttle Thermal Protection System for Impact Analyses

Published:2004-01-05 Issue: Volume: Page:
ISSN:
Container-title:42nd AIAA Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Lu Wei-Yang¹,Antoun Bonnie¹,Korellis John¹,Scheffel Simon¹,Lee Moo¹,Hardy Robert¹

Affiliation:

1. Sandia National Laboratories

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2004-945

Reference3 articles.

1. NASA Facts, Obiter Thermal Protection System, FS-2000-06-29-KSC, March1997.

2. Theoretical and experimental investigation of compaction bands in porous rock

Cited by 6 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Simulation of Orbital Debris Impact on Porous Ceramic Tiles;54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2013-04-05

2. Simulation of orbital debris impact on the Space Shuttle wing leading edge;International Journal of Impact Engineering;2006-12

3. Simulation of Hypervelocity Impact Effects on Reinforced Carbon-Carbon;Journal of Spacecraft and Rockets;2006-01

4. Simulation of Foam-Impact Effects on the Space Shuttle Thermal Protection System;Journal of Spacecraft and Rockets;2005-03

5. Analyses of Foam Impact onto the Columbia Shuttle Wing Leading Edge Panels Using Pronto3d/SPH;42nd AIAA Aerospace Sciences Meeting and Exhibit;2004-01-05

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