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2025-04-04
Temperature Dependent Design of Streamlined Ablatable Radomes for Hypersonic Applications
By
Progress In Electromagnetics Research B, Vol. 111, 59-70, 2025
Abstract
This paper presents the temperature-dependent design of streamlined constant and variable thickness ablatable radomes for hypersonic applications. An optimized three-layer radome wall configuration is proposed, consisting of a radome shell sandwiched between an outer ablative layer and an inner matching layer. The outer ablative layer offers protection against temperatures up to 1600˚F, while the inner matching layer effectively prevents total internal reflections. The radome shell is designed using the inhomogeneous planar layer model to account for the temperature gradient existing across its thickness. The numerical analysis of the radome wall is done using the 3D ray tracing method with aperture integration. Power transmission and boresight error characteristics of the radomes remain stable over a thermal operating range of 250˚F to 1600˚F. The performance of the radomes in dynamic flight conditions is analyzed using the time step analysis. Post ablation, the power transmission of constant thickness and variable thickness radomes remains well above -0.6 dB and -0.5 dB, respectively. The broadband performance of both radomes is analyzed over the X-band. Except for the boresight direction, the power transmission over the X-band remains above -1 dB for all incidence angles. The maximum boresight error is observed to be less than 4.29 mrad over the X-band.
Citation
Rudra Narayan Barik, Aparna Parameswaran, and Hrishikesh Sonalikar, "Temperature Dependent Design of Streamlined Ablatable Radomes for Hypersonic Applications," Progress In Electromagnetics Research B, Vol. 111, 59-70, 2025.
doi:10.2528/PIERB25022102
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