High‑Temperature Stealth Across Multi‑Infrared and Microwave Bands with Efficient Radiative Thermal Management

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High‑Temperature Stealth Across Multi‑Infrared and Microwave Bands with Efficient Radiative Thermal Management
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High-Temperature Stealth Across Multi-Infrared and Microwave Bands with Efficient Radiative Thermal Management - Nano-Micro Letters

High-temperature stealth is vital for enhancing the concealment, survivability, and longevity of critical assets. However, achieving stealth across multiple infrared bands—particularly in the short-wave infrared (SWIR) band—along with microwave stealth and efficient thermal management at high temperatures, remains a significant challenge. Here, we propose a strategy that integrates an IR-selective emitter (Mo/Si multilayer films) and a microwave metasurface (TiB2–Al2O3–TiB2) to enable multi-infrared band stealth, encompassing mid-wave infrared (MWIR), long-wave infrared (LWIR), and SWIR bands, and microwave (X-band) stealth at 700 °C, with simultaneous radiative cooling in non-atmospheric window (5–8 μm). At 700 °C, the device exhibits low emissivity of 0.38/0.44/0.60 in the MWIR/LWIR/SWIR bands, reflection loss below − 3 dB in the X-band (9.6–12 GHz), and high emissivity of 0.82 in 5–8 μm range—corresponding to a cooling power of 9.57 kW m−2. Moreover, under an input power of 17.3 kW m−2—equivalent to the aerodynamic heating at Mach 2.2—the device demonstrates a temperature reduction of 72.4 °C compared to a conventional low-emissivity molybdenum surface at high temperatures. This work provides comprehensive guidance on high-temperature stealth design, with far-reaching implications for multispectral information processing and thermal management in extreme high-temperature environments.

As hypersonic vehicles, scramjet nozzles and high-speed drones push beyond Mach 2, their skins glow at 700 °C—shining like a beacon in every thermal and radar band. Now, researchers from Zhejiang University and Westlake University, led by Dr. Qiang Li and Dr. Meng Zhao, have unveiled a single, scalable coating that hides platforms from SWIR, MWIR, LWIR and X-band radar while actively shedding 9.6 kW m-2 of waste heat. The work delivers a turnkey architecture for survivability in extreme flight regimes.

Why Multispectral Stealth Matters
Peak-Shift Problem: At 700 °C black-body radiation peaks at 2.8 µm—inside the short-wave IR (SWIR) window—making conventional MWIR/LWIR-only camouflage obsolete.
Radar-IR Conflict: Low-emissivity metals that suppress IR are perfect microwave reflectors, while radar absorbers glow fiercely at high temperature.
Heat-Accumulation Trap: Thick thermal insulators cool the inner airframe but cook the outer skin when aerodynamic heating strikes, leading to catastrophic IR signature spikes.

Innovative Design & Features
IR-Selective Emitter: A laser-etched Mo/Si multilayer (total < 1 µm) delivers ε ≤ 0.38/0.44/0.60 across MWIR/LWIR/SWIR yet jumps to ε = 0.82 in the 5–8 µm “non-atmospheric” window—turning the surface into a high-power radiator exactly where the sky is transparent.
TiB2 Metasurface: Embedded square blocks create an impedance-matched Salisbury screen that sucks in 9.6–12 GHz microwaves with < −3 dB reflection while surviving 700 °C in air.
Monolithic Integration: Both functional layers are deposited by standard e-beam evaporation and picosecond-laser diced on a single Al2O3 tile, enabling wafer-scale fabrication and direct bonding to curved aerosurfaces.

Applications & Future Outlook
72 °C Cooler: Under 17.3 kW m-2 aerodynamic heating (Mach 2.2 equivalent) the hybrid surface runs 72.4 °C colder than low-emissivity molybdenum, translating into a 270 °C lower radiative temperature in the LWIR band—an unambiguous “vanishing” act for thermal imagers.
Five-Band Cloaking: Experimental IR cameras confirm signal suppression of 37–64 % versus black-body references in SWIR, MWIR and LWIR up to 700 °C, while X-band radar cross-section drops by > 90 % across 2.4 GHz of bandwidth.
Beyond Hypersonics: The same stack doubles as a radiative heat sink for satellite bus panels, turbine shrouds and reusable launch-vehicle leading edges, offering a universal thermal-management skin for any high-flux, high-risk platform.

Challenges & Opportunities: The team highlights next steps—boosting SWIR emissivity below 0.5, pushing operating temperature to 1000 °C through high-entropy-ceramic spacers, and roll-to-roll transfer of the metasurface onto polymer-matrix composites for flexible hypersonic wings.

This work provides a photonics-first route to simultaneous multispectral stealth and self-cooling, promising a new generation of survivable, energy-efficient platforms for both military and civilian extreme-environment missions.

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Materials Chemistry
Physical Sciences > Chemistry > Materials Chemistry
Materials for Energy and Catalysis
Physical Sciences > Materials Science > Materials for Energy and Catalysis
Surfaces, Interfaces and Thin Film
Physical Sciences > Materials Science > Surfaces, Interfaces and Thin Film
Nanoscale Design, Synthesis and Processing
Physical Sciences > Materials Science > Nanotechnology > Nanoscale Design, Synthesis and Processing
  • Nano-Micro Letters Nano-Micro Letters

    Nano-Micro Letters is a peer-reviewed, international, interdisciplinary and open-access journal that focus on science, experiments, engineering, technologies and applications of nano- or microscale structure and system in physics, chemistry, biology, material science, and pharmacy.