Physical Challenges and Limitations Confronting the Use of UHTCs on Hypersonic Vehicles-Reference-Cited by-同舟云学术

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Physical Challenges and Limitations Confronting the Use of UHTCs on Hypersonic Vehicles

Published:2011-04-11 Issue: Volume: Page:
ISSN:
Container-title:17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
language:
Short-container-title:

Author:

Glass David¹

Affiliation:

1. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-2304

Reference42 articles.

1. Evaluation of ultra-high temperature ceramics foraeropropulsion use

2. Weight Growth Study of Reusable Launch Vehicle Systems

3. Thermal shock resistance of ZrB2 and ZrB2–30% SiC

4. High toughness, 3D textile, SiC/SiC composites by chemical vapor infiltration

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1. Multiscale structural understanding of plasma spraying anti-ablation coating: an example of Ta-Hf-W-C ultrahigh temperature ceramics;Corrosion Science;2024-07

2. Processing of Continuous Carbon Fibre Reinforced ZrB2-SiC Composite Through In-Situ Matrix Development;Transactions of the Indian Institute of Metals;2024-05-07

3. Material Research for Hypersonic Travel;International Journal of Innovative Science and Research Technology (IJISRT);2024-05-01

4. Materials design for hypersonics;Nature Communications;2024-04-18

5. Processing and characterization of 2D woven ZrB₂‐based ultrahigh‐temperature ceramic matrix composites;International Journal of Applied Ceramic Technology;2023-09-11

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