Home Journals Articles Updates About
CN
image
收藏切换
Refined Design Method of Coating Thermal Protection Structure based on Ablation Mechanism
收藏切换
PDF
Ling JIN1, Cheng ZHANG1, 2, Yadong BIAN1, Ke CHEN1, Xuanxiu LIU1
Missiles and Space Vehicles | 2024, 47(1) : 46 - 50
Less
收藏切换
Missiles and Space Vehicles | 2024, 47(1): 46-50
• Launch Vehicle and Missile •
Refined Design Method of Coating Thermal Protection Structure based on Ablation Mechanism
Full
Ling JIN1, Cheng ZHANG1, 2, Yadong BIAN1, Ke CHEN1, Xuanxiu LIU1
Affiliations
  • 1 China Academy of Launch Vehicle Technology,Beijing,100076
  • 2 College of Aerospace Science and Engineering,National University of Defense Technology,Changsha,410073
Published: 2024-02-25 doi: 10.7654/j.issn.2097-1974.20240109
Outline
收藏切换

In order to achieve lightweight, low cost and refined thermal design, the refined design method of coating thermal protection structure based on ablation mechanism is proposed. It can calculate the thickness of ablative carbon layer with using ablation mechanism, build thermal simulation model of ablation refinement and calculat accurate thermal simulation results. The application of this method can provide an effective and scientific theoretical analysis method for the demonstration of coating thermal protection scheme. It can guide the design of thermal protection scheme, reduce the design cost and shorten the development period.

ablation mechanism  /  coating  /  thermal protection structure  /  refinement  /  design method
Ling JIN, Cheng ZHANG, Yadong BIAN, Ke CHEN, Xuanxiu LIU. Refined Design Method of Coating Thermal Protection Structure based on Ablation Mechanism[J]. Missiles and Space Vehicles, 2024 , 47 (1) : 46 -50 . DOI: 10.7654/j.issn.2097-1974.20240109
Appendix
Less
Year 2024 volume 47 Issue 1
PDF
390
163
Cite this Article
BibTeX
Article Info
doi: 10.7654/j.issn.2097-1974.20240109
  • Receive Date：2022-01-20
  • Online Date：2025-07-04
  • Published：2024-02-25
Article Data
Affiliations
History
  • Received：2022-01-20
  • Revised：2023-09-08
Affiliations
    1 China Academy of Launch Vehicle Technology,Beijing,100076
    2 College of Aerospace Science and Engineering,National University of Defense Technology,Changsha,410073
References
Share
https://castjournals.cast.org.cn/joweb/ddyht/EN/10.7654/j.issn.2097-1974.20240109
Share to
QR

Scan QR to access full text

Cite this article
BibTeX
Citations
表12种不同金属材料的力学参数
科
Family		 属数
Number of
genus		 种数
Number of
species		 占总种数比例
Percentage of
total species (%)		 属
Genus		 种数
Number of
species		 占总种数比例
Percentage of total
species (%)
鹅膏菌科Amanitaceae 2 11 5.26 鹅膏菌属 Amanita 10 4.78
小菇科 Mycenaceae 2 12 5.74 丝盖伞属 Inocybe 5 2.39
多孔菌科 Polyporaceae 8 14 6.70 蜡蘑属 Laccaria 5 2.39
红菇科 Russulaceae 3 23 11.00 小皮伞属 Marasmius 6 2.87
小菇属 Mycena 11 5.26
光柄菇属 Pluteus 5 2.39
红菇属 Russula 17 8.13
栓菌属 Trametes 5 2.39
关闭全屏
  • BibTeX
  • EndNote
  • RefWorks
  • TxT
Links
Articles
Latest Articles
Most Read
Collections
Updates
Events
News
Multimedia
About
About Us
Contact
No. 86 Xueyuan South Road, Haidian District, Beijing
100081
010-62199257
qkjq@cast.org.cn

Copyright © 2025 China Association for Science and Technology. All rights reserved. For all open access content, the relevant licensing terms apply.
Sponsored by the Office of the Leading Group for Cybersecurity and Informatization of CAST, and supported by Science and Technology Review Publishing House