Design, Fabrication, and Testing of Metallic Thermal Protection Systems for Spaceplane Vehicles-Reference-Cited by-同舟云学术

Design, Fabrication, and Testing of Metallic Thermal Protection Systems for Spaceplane Vehicles

Published:2021-07 Issue:4 Volume:58 Page:1043-1060
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Le Vinh Tung¹,Goo Nam Seo¹^ORCID

Affiliation:

1. Konkuk University, Seoul 05029, Republic of Korea

Funder

Konkuk University

National Research Foundation of Korea

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.A34908

Reference36 articles.

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2. JamesonA. D. “X-37 Space Vehicle: Starting a New Age in Space Control?” NASA TR AD-A407255, 2001.

3. MyersD. E.MartinC. J.BlosserM. L. “Parametric Weight Comparison of Advanced Metallic, Ceramic Tile, and Ceramic Blanket Thermal Protection Systems,” NASA TM-2000-210289, 2000.

4. Improving Metallic Thermal Protection System Hypervelocity Impact Resistance Through Numerical Simulations

5. Development of Advanced Metallic-Thermal-Protection System Prototype Hardware

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