Computational study of hypervelocity impacts on metallic thermal protection systems-Reference-Cited by-同舟云学术

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Computational study of hypervelocity impacts on metallic thermal protection systems

Published:1998-04-27 Issue: Volume: Page:
ISSN:
Container-title:8th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
language:
Short-container-title:

Author:

Poteet Carl¹

Affiliation:

1. Joint Inst. for Advancement of Flight Sciences, Hampton, VA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1998-1611

Reference13 articles.

1. Blosser,M.L. "DevelopmentofMetallic ThermalProtectionSystemsfortheReusable LaunchVehicle,"PresentedattheSpace Technology andApplicationsInternational Forum,2ndConference onNextGeneration Launch Systems,Albuquerque,NM, 1997. Also published asNASA TM 110296, Oct.1996.

2. McGlaun,J.M.,et. al."ABrief Description of theThree-DimensionalShockWavePhysics CodeCTH,"SandiaNationalLaboratories SAND89-0607,July 1990.

3. Theoretical equation of state for aluminum

Cited by 1 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. Improving Metallic Thermal Protection System Hypervelocity Impact Resistance Through Numerical Simulations;Journal of Spacecraft and Rockets;2004-03

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