Integrated Thermal Protection System Design for Hypersonic Vehicle Based on New Thermal–Mechanical Method-Reference-Cited by-同舟云学术

Integrated Thermal Protection System Design for Hypersonic Vehicle Based on New Thermal–Mechanical Method

Published:2022-01 Issue:1 Volume:35 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Wang Yifan¹,Zhang Qing²,Tang Zhiyong³,Tian Zheng⁴,Zheng Yuning⁵^ORCID

Affiliation:

1. Senior Engineer, Science and Technology on Space Physics Laboratory, No. 1 Nandahongmen Rd., Fengtai District, Beijing 100076, China (corresponding author).

2. Engineer, Beijing Institute of Aerospace Systems Engineering, No. 1 Nandahongmen Rd., Fengtai District, Beijing 100076, China.

3. Professor, Science and Technology on Space Physics Laboratory, No. 1 Nandahongmen Rd., Fengtai District, Beijing 100076, China.

4. Senior Engineer, Science and Technology on Space Physics Laboratory, No. 1 Nandahongmen Rd., Fengtai District, Beijing 100076, China.

5. Engineer, Science and Technology on Space Physics Laboratory, No. 1 Nandahongmen Rd., Fengtai District, Beijing 100076, China. ORCID: .

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0001374

Reference29 articles.

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2. Bapanapalli S. K. 2006. “Analysis and design of corrugated-core sandwich panels for thermal protection system of space vehicles.” In Proc. 47th AIAA Structures Structural Dynamics and Materials Conf. Reston VA: American Institute of Aeronautics and Astronautics.

3. Bapanapalli S. K. 2007. “Design of an integral thermal protection system for future space vehicles.” Ph.D. thesis Pacific Northwest National Laboratory Univ. of Florida.

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

5. Bouslog, S., B. Moore, and I. Lawson. 1999. X-33 metallic TPS tests in NASA-LARC high temperature tunnel, 99–1045. Reston, VA: American Institute of Aeronautics and Astronautics.

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