Metamaterial-Based Thermal Shielding Structures for Reusable Hypersonic Space Transportation Systems

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Year : 2026 | Volume : 16 | 02 | Page :
By

Bibhu Prasad Ganthia,

Subash Ranjan Kabat,

  1. Asssitant Professor, Electrical Engineering, Indira Gandhi Institute of Technology, Sarang, Dhenkanal, Odisha, India
  2. Professor and Principal, Electrical Engineering, Radhakrishna Institute of Technology and Engineering, Bhubaneswar, Odisha, India

Abstract

The rapid development of reusable hypersonic space transportation systems has intensified the need for advanced thermal protection technologies capable of withstanding extreme aerodynamic heating conditions encountered during atmospheric re-entry and sustained hypersonic flight. Conventional thermal shielding materials often suffer from high structural weight, limited adaptability, thermal fatigue, and degradation under repeated thermal cycling. This study proposes a novel Metamaterial-Based Thermal Shielding Structure for Reusable Hypersonic Space Transportation Systems, integrating engineered metamaterial architectures with ultra-high- temperature ceramic composites and multifunctional heat management mechanisms to achieve superior thermal protection performance. The proposed structure utilizes periodic micro-lattice geometries and tunable electromagnetic properties to manipulate heat transfer pathways through radiation suppression, phononic wave attenuation, and adaptive thermal dissipation. Numerical simulations under Mach 8–15 flight conditions demonstrate a reduction in surface temperature by approximately 27.8%, improvement in thermal resistance by 34.6%, and enhancement of thermal cycling durability by 41.3% compared with conventional ceramic thermal protection systems. Furthermore, the lightweight metamaterial design achieves a mass reduction of 18.5%, contributing to improved payload capacity and fuel efficiency. The integration of artificial intelligence-assisted thermal prediction models further enables real-time structural health monitoring and predictive maintenance. The proposed approach offers a promising pathway toward sustainable, reusable, and high-performance thermal protection solutions for future hypersonic aerospace transportation systems.

Keywords: Metamaterials; Thermal Protection Systems; Hypersonic Vehicles; Reusable Space Transportation; Ultra-High-Temperature Ceramics; Aerospace Structures.

How to cite this article:
Bibhu Prasad Ganthia, Subash Ranjan Kabat. Metamaterial-Based Thermal Shielding Structures for Reusable Hypersonic Space Transportation Systems. Journal of Aerospace Engineering & Technology. 2026; 16(02):-.
How to cite this URL:
Bibhu Prasad Ganthia, Subash Ranjan Kabat. Metamaterial-Based Thermal Shielding Structures for Reusable Hypersonic Space Transportation Systems. Journal of Aerospace Engineering & Technology. 2026; 16(02):-. Available from: https://journals.stmjournals.com/joaet/article=2026/view=250432

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Ahead of Print Subscription Review Article
Volume 16
02
Received 15/07/2026
Accepted 16/07/2026
Published 22/07/2026
Publication Time 7 Days


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